OBJECT B, 61870
Orbit data source: Space-Track
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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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: 7 hours ago
TLE from 7 hours ago
0 OBJECT B
1 61870U 24203B 26133.93869824 .00009761 00000-0 34498-3 0 9991
2 61870 97.4195 204.3218 0013010 89.8452 270.4279 15.29317087 83735Epoch: 2026-05-13T22:31Z
TLE epoch observation values (Epoch: 2026-05-13T22:31:43.527Z)
Latitude
-0.00005°
Longitude
-5.30109°
Altitude
480.9 km
Speed
7.625 km/s
True Right ascension
13h 37m 17s
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
14:03:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.722 km
Perigee altitude
465.891 km
Semi-major axis
6,852.944 km
Eccentricity
0.0013
Inclination
97.4195°
RAAN
204.3218°
Arg. of periapsis
89.8452°
True anomaly
270.27882°
Mean anomaly
270.4279°
Eccentric anomaly
270.35336°
Mean motion
3.82585 °/min
Orbital period
94.1 mins
BSTAR
0.00034498
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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 | 2026-05-14 17:55:43.653Z | 354.604° N | 2026-05-14 17:58:43.653Z | 276.359° WNW | 33.505° | 2026-05-14 18:01:43.653Z | 215.238° SW |
| 5 mins | 2026-05-15 04:30:43.653Z | 145.448° SSE | 2026-05-15 04:32:43.653Z | 61.577° ENE | 39.655° | 2026-05-15 04:35:43.653Z | 357.497° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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