OV1-10 R/B, 2621
Orbit data source: Space-Track
OV1-10 R/B, 2621 is space debris in LEO originally from a launch on Sun, 11 Dec 1966 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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2621 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
125 kg wet, 125 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OV1-10 R/B
1 2621U 66111C 25356.10589757 .00000832 00000-0 95381-4 0 9992
2 2621 93.3998 129.4449 0055638 342.2701 17.6580 14.85222614148075Epoch: 2025-12-22T02:32Z
TLE epoch observation values (Epoch: 2025-12-22T02:32:29.550Z)
Latitude
0.00001°
Longitude
0.41301°
Altitude
578.961 km
Speed
7.591 km/s
True Right ascension
08h 37m 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
09:11:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
648.655 km
Perigee altitude
570.896 km
Semi-major axis
6,987.913 km
Eccentricity
0.00556
Inclination
93.3998°
RAAN
129.4449°
Arg. of periapsis
342.2701°
True anomaly
17.85268°
Mean anomaly
17.658°
Eccentric anomaly
17.75521°
Mean motion
3.71554 °/min
Orbital period
96.89 mins
BSTAR
0.000095381
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Other satellites on launch #111 in the year 1966 (1966-12-11 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.OV1-10 R/B Visibility forecast
Loading observer location...
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 | 2025-12-22 20:54:13.157Z | 35.088° NE | 2025-12-22 20:57:13.157Z | 82.04° E | 24.412° | 2025-12-22 21:01:13.157Z | 147.402° SSE |
| 5 mins | 2025-12-22 22:32:13.157Z | 318.972° NNW | 2025-12-22 22:34:13.157Z | 278.401° WNW | 23.272° | 2025-12-22 22:37:13.157Z | 232.897° WSW |
| 6 mins | 2025-12-23 09:24:13.157Z | 181.083° SSW | 2025-12-23 09:26:13.157Z | 224.419° SW | 43.693° | 2025-12-23 09:30:13.157Z | 349.599° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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