OBJECT BC, 63260
Orbit data source: Space-Track
OBJECT BC, 63260 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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63260 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
Yonsei U
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 4 Pan + 1 Sail, 0.5 m
Radar Cross Section
0.090 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OBJECT BC
1 63260U 25052BC 26264.94748062 .00000460 00000-0 47273-4 0 9998
2 63260 97.6692 154.2691 0002431 46.8395 313.3028 14.94904836 83088Epoch: 2026-09-21T22:44Z
TLE epoch observation values (Epoch: 2026-09-21T22:44:22.325Z)
Latitude
-0.00009°
Longitude
172.35609°
Altitude
584.556 km
Speed
7.569 km/s
True Right ascension
10h 17m 04s
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
11:59:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.37 km
Perigee altitude
577.987 km
Semi-major axis
6,957.816 km
Eccentricity
0.00024
Inclination
97.6692°
RAAN
154.2691°
Arg. of periapsis
46.8395°
True anomaly
313.28252°
Mean anomaly
313.3028°
Eccentric anomaly
313.29266°
Mean motion
3.73967 °/min
Orbital period
96.27 mins
BSTAR
0.000047273
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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 BC 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-23 05:49:08.059Z | 4.793° NNE | 2026-09-23 05:53:08.059Z | 267.696° W | 61.825° | 2026-09-23 05:56:08.059Z | 206.683° SW |
| 6 mins | 2026-09-23 16:39:08.059Z | 156.09° SSE | 2026-09-23 16:41:08.059Z | 95.397° ESE | 73.258° | 2026-09-23 16:45:08.059Z | 351.877° 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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