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: 4 days ago

TLE from 4 days ago

0 H-2A R/B
1 27369U 02003C   26205.92512264  .00000043  00000-0  00000-0 0  9995
2 27369  23.6967 130.6695 6881869 266.4264  19.3824  2.37191541211406

Epoch: 2026-07-24T22:12Z

TLE epoch observation values (Epoch: 2026-07-24T22:12:10.596Z)

Latitude

0.00041°

Longitude

-145.10217°

Altitude

6,704.281 km

Speed

6.645 km/s

True Right ascension

08h 42m 20s

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

11:34:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

33,723.039 km

Perigee altitude

1,028.669 km

Semi-major axis

23,753.991 km

Eccentricity

0.68819

Inclination

23.6967°

RAAN

130.6695°

Arg. of periapsis

266.4264°

True anomaly

93.69591°

Mean anomaly

19.3824°

Eccentric anomaly

49.25607°

Mean motion

0.59284 °/min

Orbital period

607.25 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.
232 mins	2026-07-28 22:08:23.347Z	97.146° ESE	2026-07-28 23:48:23.347Z	104.393° ESE	34.658°	2026-07-29 02:00:23.347Z	105.932° 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: 4 days ago

TLE from 4 days ago

TLE epoch observation values (Epoch: 2026-07-24T22:12:10.596Z)

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: 4 days ago