H-3 R/B, 62877
Orbit data source: Space-Track
H-3 R/B, 62877 is space debris in HEO originally from a launch on Sun, 02 Feb 2025 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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62877 intel report (Beta)
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Edit Public Description
| Identifier | |
| Orbit | HEO |
| Last TLE update | 15 hours ago |
| Origin | |
| Manufacturer | MHI Tobishima |
| Mission | Spacecraft |
| Bus & Motor | H-2A STAGE 2, Unknown motor |
| Mass | 2,500 kg wet, 2,500 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | RCS unknown |
Expand to show TLE details & history
TLE from 15 hours ago
0 H-3 R/B
1 62877U 25023B 25070.54392810 .00006154 00000-0 17281-2 0 9995
2 62877 21.2854 289.1629 7247089 201.7285 96.0877 2.32406973 871Epoch: 2025-03-11T13:03Z
Definitive object data (Epoch: 2025-03-11T13:03:15.387Z)
| Latitude | -0.0002° |
| Longitude | -76.12521° |
| Altitude | 28,557.294 km |
| Speed | 2.503 km/s |
| True Right ascension | 19h 16m 32s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 15.68646° |
| Longitude | -30.18711° |
| Altitude | 26,434.02 km |
| Speed | 2.782 km/s |
| Apparent Right ascension | 22h 08m 40s |
| Apparent Declination | 7° 32' 27" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:52:27 |
| Azimuth | 335.244° NNW |
| Elevation | -39.381° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 35,152.259 km |
| Perigee altitude | 250.778 km |
| Semi-major axis | 24,079.656 km |
| Eccentricity | 0.7247089 |
| Inclination | 21.2854° |
| RAAN | 289.1629° |
| Arg. of periapsis | 201.7285° |
| True anomaly | 158.21239° |
| Mean anomaly | 96.0877° |
| Eccentric anomaly | 128.5577° |
| Mean motion | 0.58086 °/min |
| BSTAR | 0.0017281 |
| Orbital period | 619.78 mins |
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Other satellites on launch #23 in the year 2025 (2025-02-02 UTC)
| QZS-6, 62876 |
H-3 R/B Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 320 mins | 2025-03-12 11:11:36.134Z | 99.228° ESE | 2025-03-12 15:07:36.134Z | 106.376° ESE | 29.047° | 2025-03-12 16:31:36.134Z | 89.222° E |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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