OBJECT A, 64087
Orbit data source: Space-Track
OBJECT A, 64087 is a Chinese satellite in SSO that was launched on Wed, 21 May 2025 UTC via a LIJIAN-1 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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64087 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Radar Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 3 Pan, 1.1 m
Radar Cross Section
3.533 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OBJECT A
1 64087U 25108A 26171.51726826 .00003550 00000-0 18708-3 0 9995
2 64087 97.4762 246.1923 0001173 300.2900 59.8217 15.16231404 59828Epoch: 2026-06-20T12:24Z
TLE epoch observation values (Epoch: 2026-06-20T12:24:51.977Z)
Latitude
-0.00001°
Longitude
151.24497°
Altitude
519.919 km
Speed
7.604 km/s
True Right ascension
16h 24m 46s
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
07:18:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.025 km
Perigee altitude
513.408 km
Semi-major axis
6,892.354 km
Eccentricity
0.00012
Inclination
97.4762°
RAAN
246.1923°
Arg. of periapsis
300.29°
True anomaly
59.83332°
Mean anomaly
59.8217°
Eccentric anomaly
59.82751°
Mean motion
3.79308 °/min
Orbital period
94.91 mins
BSTAR
0.00018708
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Other satellites on launch #108 in the year 2025 (2025-05-21 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 | 2026-06-21 04:24:04.813Z | 121.15° SE | 2026-06-21 04:26:04.813Z | 78.86° E | 24.941° | 2026-06-21 04:29:04.813Z | 15.777° NNE |
| 6 mins | 2026-06-21 17:30:04.813Z | 33.575° NE | 2026-06-21 17:32:04.813Z | 78.26° E | 33.533° | 2026-06-21 17:36:04.813Z | 172.045° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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