OBJECT E, 63986
Orbit data source: Space-Track
OBJECT E, 63986 is a Chinese satellite in SSO that was launched on Wed, 14 May 2025 UTC via a CHANG ZHENG 2D 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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63986 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.135 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OBJECT E
1 63986U 25100E 26206.62650484 .00012473 00000-0 56518-3 0 9996
2 63986 97.3615 278.4751 0011588 174.2440 185.8931 15.20934295 36299Epoch: 2026-07-25T15:02Z
TLE epoch observation values (Epoch: 2026-07-25T15:02:10.018Z)
Latitude
-0.00001°
Longitude
109.59728°
Altitude
514.048 km
Speed
7.602 km/s
True Right ascension
18h 33m 54s
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
15:23:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.954 km
Perigee altitude
492.013 km
Semi-major axis
6,878.121 km
Eccentricity
0.00116
Inclination
97.3615°
RAAN
278.4751°
Arg. of periapsis
174.244°
True anomaly
185.87949°
Mean anomaly
185.8931°
Eccentric anomaly
185.88629°
Mean motion
3.80486 °/min
Orbital period
94.62 mins
BSTAR
0.00056518
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Other satellites on launch #100 in the year 2025 (2025-05-14 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 E 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 | 2026-07-26 05:23:25.294Z | 211.402° SW | 2026-07-26 05:25:25.294Z | 272.564° WNW | 30.059° | 2026-07-26 05:28:25.294Z | 329.199° NNW |
| 4 mins | 2026-07-26 18:27:25.294Z | 324.085° NNW | 2026-07-26 18:28:25.294Z | 301.433° NW | 21.674° | 2026-07-26 18:31:25.294Z | 238.635° WSW |
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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