OBJECT B, 61870
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT B, 61870 is a satellite owned by Hangtian Hongtu (CN) in SSO that was launched on Sat, 09 Nov 2024 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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61870 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Yinhe
Mission
Operational Commercial Radar Imaging
Bus & Motor
PIESAT, Unknown motor
Mass
270 kg wet, 270 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
2.315 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 hours ago
TLE from 3 hours ago
0 OBJECT B
1 61870U 24203B 25257.30352956 .00007902 00000-0 35498-3 0 9997
2 61870 97.4530 324.1039 0012944 210.9361 149.1113 15.21350817 46896Epoch: 2025-09-14T07:17Z
TLE epoch observation values (Epoch: 2025-09-14T07:17:04.953Z)
Latitude
-0.00011°
Longitude
-138.69119°
Altitude
512.503 km
Speed
7.603 km/s
True Right ascension
21h 36m 24s
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
03:13:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.633 km
Perigee altitude
489.83 km
Semi-major axis
6,876.868 km
Eccentricity
0.00129
Inclination
97.453°
RAAN
324.1039°
Arg. of periapsis
210.9361°
True anomaly
149.18734°
Mean anomaly
149.1113°
Eccentric anomaly
149.14933°
Mean motion
3.8059 °/min
Orbital period
94.59 mins
BSTAR
0.00035498
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Other satellites on launch #203 in the year 2024 (2024-11-09 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.OBJECT 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-14 17:18:52.864Z | 15.838° NNE | 2025-09-14 17:21:52.864Z | 53.592° ENE | 42.992° | 2025-09-14 17:24:52.864Z | 186.167° SSW |
| 4 mins | 2025-09-15 03:57:52.864Z | 111.801° ESE | 2025-09-15 03:59:52.864Z | 58.993° ENE | 24.709° | 2025-09-15 04:01:52.864Z | 19.065° NNE |
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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