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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27369 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated 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)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 4.6 m
Radar Cross Section
35.186 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 H-2A R/B
1 27369U 02003C 25260.58261323 -.00000111 00000-0 00000-0 0 9991
2 27369 23.7086 234.0968 6882349 87.4864 343.1026 2.37190006204030Epoch: 2025-09-17T13:58Z
TLE epoch observation values (Epoch: 2025-09-17T13:58:57.783Z)
Latitude
0.00004°
Longitude
27.48271°
Altitude
5,749.37 km
Speed
6.996 km/s
True Right ascension
15h 35m 55s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:18:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,724.352 km
Perigee altitude
1,027.56 km
Semi-major axis
23,754.093 km
Eccentricity
0.68823
Inclination
23.7086°
RAAN
234.0968°
Arg. of periapsis
87.4864°
True anomaly
272.71483°
Mean anomaly
343.1026°
Eccentric anomaly
315.4287°
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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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.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. |
|---|---|---|---|---|---|---|---|
| 348 mins | 2025-09-18 14:27:49.862Z | 160.741° S | 2025-09-18 19:22:49.862Z | 172.038° S | 17.504° | 2025-09-18 20:15:49.862Z | 138.279° SSE |
| 14 mins | 2025-09-19 07:00:49.862Z | 217.827° SW | 2025-09-19 07:04:49.862Z | 174.986° S | 20.332° | 2025-09-19 07:14:49.862Z | 131.17° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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