H-2A R/B, 27369

Orbit data source: Space-Track

H-2A R/B, 27369 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/27369?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

27369, 2002-003C

Orbit

HEO

Country

JP / JPN

Related business

JAXA (Japan Aerospace Exploration Agency) (JP)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

H-2A STAGE 2, Unknown motor

Mass

4,000 kg wet, 4,000 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

Cyl, 4.6 m

Radar Cross Section

35.186 m², Large (>1 m²)

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Last TLE update: 17 hours ago

TLE from 17 hours ago

0 H-2A R/B
1 27369U 02003C   26089.24936611 -.00000209  00000-0  00000-0 0  9991
2 27369  23.8056 169.7154 6852780 198.9630 111.4718  2.37191020208635

Epoch: 2026-03-30T05:59Z

TLE epoch observation values (Epoch: 2026-03-30T05:59:05.231Z)

Latitude

0.00018°

Longitude

-107.63833°

Altitude

29,450.82 km

Speed

2.338 km/s

True Right ascension

11h 19m 06s

True Declination

0° 00' 01"

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

04:25:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

33,653.913 km

Perigee altitude

1,097.761 km

Semi-major axis

23,753.974 km

Eccentricity

0.68528

Inclination

23.8056°

RAAN

169.7154°

Arg. of periapsis

198.963°

True anomaly

161.08075°

Mean anomaly

111.4718°

Eccentric anomaly

137.83046°

Mean motion

0.59284 °/min

Orbital period

607.24 mins

BSTAR

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Computing Atmospheric mass density...

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

H-2A DEB, 43371 (Decayed)

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H-2A R/B 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.
438 mins	2026-03-31 01:18:22.871Z	116.956° SE	2026-03-31 07:06:22.871Z	121.757° SE	37.089°	2026-03-31 08:36:22.871Z	89.572° E

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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 R/B, 27369 on other resources

View H-2A R/B, 27369 on Heavens-Above

View H-2A R/B, 27369 on Keep Track

View H-2A R/B, 27369 on Celestrak

View H-2A R/B, 27369 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 R/B, 27369

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-03-30T05:59:05.231Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

H-2A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-2A R/B, 27369 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago