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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Identifier
27369, 2002-003C
Orbit
HEO
Country
Flag of JPJP / JPN
Related business
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 (25 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 5.0 m
Radar Cross Section
35.186 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago
0 H-2A R/B
1 27369U 02003C   26266.20187458 -.00000012  00000-0  00000-0 0  9993
2 27369  23.7881 110.0865 6894624 301.6624   8.9929  2.37189674212830
Epoch: 2026-09-23T04:50Z
TLE epoch observation values (Epoch: 2026-09-23T04:50:41.963Z)
Latitude
0.00019°
Longitude
35.46132°
Altitude
2,792.773 km
Speed
8.375 km/s
True Right ascension
07h 20m 46s
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
18:12:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,753.565 km
Perigee altitude
998.412 km
Semi-major axis
23,754.125 km
Eccentricity
0.68946
Inclination
23.7881°
RAAN
110.0865°
Arg. of periapsis
301.6624°
True anomaly
58.13939°
Mean anomaly
8.9929°
Eccentric anomaly
26.81051°
Mean motion
0.59284 °/min
Orbital period
607.25 mins
BSTAR
0
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Other satellites on launch #3 in the year 2002 (2002-02-04 UTC)

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