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
Country
JP / JPNRelated business
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
Shape & HBR
Cyl, 5.6 m
Radar Cross Section
55.543 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 H-3 R/B
1 62877U 25023B 25297.74418508 .00003395 00000-0 25668-2 0 9993
2 62877 20.9964 198.3821 7213054 3.6853 359.6952 2.33750617 6178Epoch: 2025-10-24T17:51Z
TLE epoch observation values (Epoch: 2025-10-24T17:51:37.590Z)
Latitude
-0.0004°
Longitude
-102.88619°
Altitude
291.537 km
Speed
10.144 km/s
True Right ascension
13h 13m 37s
True Declination
0° 00' 01"
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
01:22:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,911.305 km
Perigee altitude
306.99 km
Semi-major axis
23,987.284 km
Eccentricity
0.72131
Inclination
20.9964°
RAAN
198.3821°
Arg. of periapsis
3.6853°
True anomaly
357.28284°
Mean anomaly
359.6952°
Eccentric anomaly
358.9065°
Mean motion
0.58421 °/min
Orbital period
616.21 mins
BSTAR
0.0025668
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Other satellites on launch #23 in the year 2025 (2025-02-02 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-3 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. |
|---|---|---|---|---|---|---|---|
| 289 mins | 2025-10-25 06:07:25.931Z | 228.274° WSW | 2025-10-25 06:07:25.931Z | 228.274° WSW | 33.289° | 2025-10-25 10:56:25.931Z | 242.848° WSW |
| 309 mins | 2025-10-26 00:58:25.931Z | 241.223° WSW | 2025-10-26 01:19:25.931Z | 173.409° S | 39.337° | 2025-10-26 06:07:25.931Z | 175.433° S |
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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