H-2A DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite H-2A DEB at a glance.

Uptime

2694

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.3

Latest

Satellite identification and parameters

Extended collection of information and parameters for H-2A DEB.

Object identification

Identified? True

Debris? True

Object name: H-2A DEB

International designator: 2017-082E

Object number (NORAD): 43069

Object ID (CCSDS): 43069

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.088 minutes

Inclination: 98.2855 deg

SMA: 7093.199 km

Apoapsis: 731.133 km

Periapsis: 698.995 km

RAAN: 194.1543 deg

Eccentricy: 0.0022654

Argument of periapsis: 303.453 deg

Mean anomaly: 56.45 deg

Mean motion: 14.53247265 rev/day

Mean motion (dot): 0.00004302 rev/day2

B* drag term: 0.0010443 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 5:25 p.m. UTC

TLE line 0: 0 H-2A DEB

TLE line 1: 1 43069U 17082E 25127.72629383 .00004302 00000-0 10443-2 0 9990

TLE line 2: 2 43069 98.2855 194.1543 0022654 303.4530 56.4500 14.53247265387765

Live tracking on map

Real-time ground track for satellite H-2A DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object H-2A DEB.

Target Orbit TCA Probability of collision Miss distance Type
THOR BURNER 2 R/B SSO 2024-08-19 16:02:44 0.0003880356 82.0 (m) ROCKET BODY
TITAN 3C TRANSTAGE DEB LEO 2024-07-30 13:00:04 0.0001957731 142.0 (m) DEBRIS

Associated space launch

GCOM-C1 is another satellite in JAXA's Earth observation Global Change Observation Mission (GCOM) constellation. This spacecraft is the first satellite in GCOM-C series and is intended to operate in sun-synchronous orbit for 5 years. It aims to collect surface and atmospheric measurements in order to monitor global climate change. Along with it is launched an engineering test satellite SLATS (Super Low Altitude Test Satellite), which is an attempt to develop techniques to operate a satellite in extremely low orbits. SLATS will try achieve that by maintaining position in orbit via ion engines. It will also collect data on atmosphere density and measure atomic oxygen in such low altitudes.

H-2A DEB was lifted into orbit during the mission ‘H-IIA 202 | GCOM-C1 & SLATS’, on board a H-IIA space rocket.

The launch took place on Dec. 23, 2017, 1:26 a.m. from Yoshinobu Launch Complex LP-1.

For more information about the launch, click the button.

Launch to space H-IIA 202 | GCOM-C1 & SLATS
H-IIA 202 | GCOM-C1 & SLATS

Agency: N/A

Status: Launch Successful

Launch date: Dec. 23, 2017, 1:26 a.m. UTC

Rocket: H-IIA

Launch pad: Yoshinobu Launch Complex LP-1

Location: Tanegashima Space Center, Japan

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