OBJECT A, 61869
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 A, 61869 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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61869 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
320 kg wet, 320 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: 16 hours ago
TLE from 16 hours ago
0 OBJECT A
1 61869U 24203A 25261.34442286 .00010702 00000-0 48066-3 0 9997
2 61869 97.4552 328.1015 0013841 198.6642 161.4088 15.21254200 47503Epoch: 2025-09-18T08:15Z
TLE epoch observation values (Epoch: 2025-09-18T08:15:58.135Z)
Latitude
0.00001°
Longitude
-153.39809°
Altitude
514.176 km
Speed
7.602 km/s
True Right ascension
21h 52m 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
17:27:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.541 km
Perigee altitude
489.504 km
Semi-major axis
6,877.16 km
Eccentricity
0.00138
Inclination
97.4552°
RAAN
328.1015°
Arg. of periapsis
198.6642°
True anomaly
161.45928°
Mean anomaly
161.4088°
Eccentric anomaly
161.43405°
Mean motion
3.80566 °/min
Orbital period
94.6 mins
BSTAR
0.00048066
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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 A 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-19 04:55:30.274Z | 194.138° SSW | 2025-09-19 04:57:30.274Z | 247.908° W | 36.065° | 2025-09-19 05:00:30.274Z | 331.608° NNW |
| 5 mins | 2025-09-19 17:59:30.274Z | 336.892° NNW | 2025-09-19 18:01:30.274Z | 283.377° WNW | 27.408° | 2025-09-19 18:04:30.274Z | 225.41° WSW |
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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