H-2A DEB, 28243

Orbit data source: Space-Track

H-2A DEB, 28243 is space debris in HEO originally from a launch on Mon, 04 Feb 2002 UTC launched from the Tanegashima Space Center (TNSTA). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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https://www.satcat.com/sats-embedded/28243?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

28243, 2002-003E

Orbit

HEO

Country

JP / JPN

Related business

JAXA (Japan Aerospace Exploration Agency) (JP)

Manufacturer

MHI Tobishima

Mission

Spacecraft

Bus & Motor

Unknown

Mass

~200 kg wet, ~200 kg dry

Launch date (UTC)

2002-02-04 (24 years ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Half Cyl, 2.0 m

Radar Cross Section

13.425 m², Large (>1 m²)

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Last TLE update: 3 months ago

TLE from 3 months ago

0 H-2A DEB
1 28243U 02003E   25262.24011465  .00024465  00000-0  52535-1 0  9996
2 28243  28.6946 272.4616 7045569 273.0127  15.3811  2.50007476199236

Epoch: 2025-09-19T05:45Z

TLE epoch observation values (Epoch: 2025-09-19T05:45:45.905Z)

Latitude

-0.00043°

Longitude

-172.36983°

Altitude

4,751.851 km

Speed

7.365 km/s

True Right ascension

18h 09m 50s

True Declination

0° 00' 02"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

13:23:56

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

32,715.991 km

Perigee altitude

397.871 km

Semi-major axis

22,935.068 km

Eccentricity

0.70456

Inclination

28.6946°

RAAN

272.4616°

Arg. of periapsis

273.0127°

True anomaly

86.56458°

Mean anomaly

15.3811°

Eccentric anomaly

42.81838°

Mean motion

0.62487 °/min

Orbital period

576.12 mins

BSTAR

0.052535

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Other satellites on launch #3 in the year 2002 (2002-02-04 UTC)

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H-2A DEB Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
496 mins	2025-12-15 20:46:21.631Z	228.306° WSW	2025-12-15 21:04:21.631Z	151.974° SSE	41.472°	2025-12-16 05:02:21.631Z	148.728° SSE

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out H-2A DEB, 28243 on other resources

View H-2A DEB, 28243 on Heavens-Above

View H-2A DEB, 28243 on Keep Track

View H-2A DEB, 28243 on Celestrak

View H-2A DEB, 28243 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

H-2A DEB, 28243

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 months ago

TLE from 3 months ago

TLE epoch observation values (Epoch: 2025-09-19T05:45:45.905Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #3 in the year 2002 (2002-02-04 UTC)

H-2A DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-2A DEB, 28243 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 months ago