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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Iframe URL

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: 18 hours ago

TLE from 18 hours ago

0 H-2A R/B
1 27369U 02003C   26149.03596605  .00000012  00000-0  00000-0 0  9991
2 27369  23.7540 149.8364 6865856 233.4432  42.2980  2.37191833210050

Epoch: 2026-05-29T00:51Z

TLE epoch observation values (Epoch: 2026-05-29T00:51:47.466Z)

Latitude

-0.00028°

Longitude

-109.76001°

Altitude

14,818.658 km

Speed

4.564 km/s

True Right ascension

09h 59m 02s

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

04:41:56

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

33,684.921 km

Perigee altitude

1,066.691 km

Semi-major axis

23,753.943 km

Eccentricity

0.68659

Inclination

23.754°

RAAN

149.8364°

Arg. of periapsis

233.4432°

True anomaly

126.57591°

Mean anomaly

42.298°

Eccentric anomaly

81.17025°

Mean motion

0.59284 °/min

Orbital period

607.24 mins

BSTAR

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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.
503 mins	2026-05-29 20:57:06.582Z	120.948° SE	2026-05-30 03:24:06.582Z	109.804° ESE	37.349°	2026-05-30 05:20:06.582Z	95.441° ESE

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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: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2026-05-29T00:51:47.466Z)

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: 18 hours ago