H-2A R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite H-2A R/B at a glance.

Uptime

4741

Days in orbit

Revolutions

≈ 14.9

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for H-2A R/B.

Object identification

Identified? True

Debris? False

Object name: H-2A R/B

International designator: 2012-025E

Object number (NORAD): 38341

Object ID (CCSDS): 38341

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 96.461 minutes

Inclination: 98.4356 deg

SMA: 6967.231 km

Apoapsis: 620.824 km

Periapsis: 557.367 km

RAAN: 69.1615 deg

Eccentricy: 0.004554

Argument of periapsis: 223.9065 deg

Mean anomaly: 135.853 deg

Mean motion: 14.92837347 rev/day

Mean motion (dot): 0.0000287 rev/day2

B* drag term: 0.00027819 1/REarth

Two-line elements (TLE)

Creation date: May 10, 2025, 2:32 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 9, 2025, 9:38 p.m. UTC

TLE line 0: 0 H-2A R/B

TLE line 1: 1 38341U 12025E 25129.90152208 .00002870 00000-0 27819-3 0 9992

TLE line 2: 2 38341 98.4356 69.1615 0045540 223.9065 135.8530 14.92837347702865

Live tracking on map

Real-time ground track for satellite H-2A R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object H-2A R/B.

Target Orbit TCA Probability of collision Miss distance Type
IRIDIUM 33 DEB LEO 2025-02-06 10:19:06 0.0001703204 760.0 (m) DEBRIS
CZ-4 DEB SSO 2024-06-29 19:47:46 0.001510107 37.0 (m) DEBRIS
SL-14 R/B LEO 2024-06-19 12:14:35 0.0002165657 153.0 (m) ROCKET BODY

Associated space launch

The GCOM-W (Global Change Observation Mission - Water) or Shizuku satellite aims to construct, use, and verify systems that enable continuous global-scale observations (for 10 to 15 years) of effective geophysical parameters for elucidating global climate change and water circulation mechanisms. Water circulation changes will be observed by a microwave radiometer onboard the GCOM-W (Water) satellite (scheduled to be launched in Japan Fiscal Year 2011). The GCOM-W will observe precipitation, vapor amounts, wind velocity above the ocean, sea water temperatures, water levels on land areas and snow depths. Climate change observation will be performed by a multi-wavelength optical radiometer onboard the GCOM-C (Climate) satellite (under consideration) on clouds, aerosol, seawater color (marine organisms), vegetation, snow and ice. These satellites will enable us to perform comprehensive observations of the surface layer of the Earth such as the atmosphere, including clouds, land, oceans and the cryosphere. The Advanced Microwave Scanning Radiometer 2 (AMSR2) is a sensor to observe radiometers, or microwaves emitted naturally from the ground, sea surface and atmosphere, using 6 different frequency bands ranging from 7 GHz to 89 GHz. The strength of a natural microwave is determined by its characteristics and moisture, including the surface condition and temperature of the material. Although it depends on the frequency, the microwave is very weak. AMSR2 will detect such weak microwaves at an altitude of 700 kilometers and measure the strength of them with a very high accuracy. For example, by measuring the strength of a microwave emitted from the sea surface with the AMSR2, one can understand the water temperature of the sea surface to an accuracy of 0.5 degrees Celsius.

H-2A R/B was lifted into orbit during the mission ‘H-IIA 202 | GCOM-W1’, on board a H-IIA space rocket.

The launch took place on May 17, 2012, 4:39 p.m. from Yoshinobu Launch Complex LP-1.

For more information about the launch, click the button.

Launch to space H-IIA 202 | GCOM-W1
H-IIA 202 | GCOM-W1

Agency: N/A

Status: Launch Successful

Launch date: May 17, 2012, 4:39 p.m. UTC

Rocket: H-IIA

Launch pad: Yoshinobu Launch Complex LP-1

Location: Tanegashima Space Center, Japan

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