OBJECT B, 63211
Orbit data source: Space-Track
OBJECT B, 63211 is a satellite in SSO that was launched on Sat, 15 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63211 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
NUSHS
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 OBJECT B
1 63211U 25052B 26120.66737334 .00021514 00000-0 65275-3 0 9998
2 63211 97.4041 17.8175 0001023 229.9236 130.1917 15.34126483 62858Epoch: 2026-04-30T16:01Z
TLE epoch observation values (Epoch: 2026-04-30T16:01:01.056Z)
Latitude
-0.00005°
Longitude
-81.04758°
Altitude
467.078 km
Speed
7.633 km/s
True Right ascension
01h 11m 16s
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
18:13:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.163 km
Perigee altitude
459.764 km
Semi-major axis
6,838.6 km
Eccentricity
0.0001
Inclination
97.4041°
RAAN
17.8175°
Arg. of periapsis
229.9236°
True anomaly
130.20065°
Mean anomaly
130.1917°
Eccentric anomaly
130.19618°
Mean motion
3.83789 °/min
Orbital period
93.8 mins
BSTAR
0.00065275
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Other satellites on launch #52 in the year 2025 (2025-03-15 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 | 2026-05-01 17:11:30.409Z | 169.217° S | 2026-05-01 17:14:30.409Z | 327.505° NNW | 44.116° | 2026-05-01 17:17:30.409Z | 346.845° N |
| 5 mins | 2026-05-02 06:09:30.409Z | 0.93° NNE | 2026-05-02 06:11:30.409Z | 280.965° WNW | 42.375° | 2026-05-02 06:14:30.409Z | 202.664° SW |
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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