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

8400

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.3

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: 2002-056E

Object number (NORAD): 27601

Object ID (CCSDS): 27601

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.441 minutes

Inclination: 98.3063 deg

SMA: 7157.609 km

Apoapsis: 830.571 km

Periapsis: 728.376 km

RAAN: 304.9613 deg

Eccentricy: 0.00713893

Argument of periapsis: 62.7669 deg

Mean anomaly: 308.8492 deg

Mean motion: 14.33675444 rev/day

Mean motion (dot): 0.00000585 rev/day2

B* drag term: 0.00021927852 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 4:22 a.m. UTC

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

TLE line 1: 1 27601U 02056E 25346.18252755 .00000585 00000-0 21928-3 0 9997

TLE line 2: 2 27601 98.3063 304.9613 0071389 62.7669 308.8492 14.33675444201577

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
CZ-6A DEB SSO 2025-09-03 15:16:09 0.0006491075 17.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-31 12:10:56 0.00013732 887.0 (m) DEBRIS
CZ-6A DEB LEO 2024-11-09 07:04:20 0.0009222718 429.0 (m) DEBRIS

Associated space launch

Midori II has been engaged in various observation missions to understand the realities and causes of global environmental changes, such as abnormal weather conditions and the expansion of the ozone hole.

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

The launch took place on Dec. 14, 2002, 1:31 a.m. from Yoshinobu Launch Complex LP-1.

For more information about the launch, click the button.

Launch to space H-IIA 202 | Midori-2
H-IIA 202 | Midori-2

Agency: N/A

Status: Launch Successful

Launch date: Dec. 14, 2002, 1:31 a.m. UTC

Rocket: H-IIA

Launch pad: Yoshinobu Launch Complex LP-1

Location: Tanegashima Space Center, Japan

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