OV1-9 R/B, 2622
Orbit data source: Space-Track
OV1-9 R/B, 2622 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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2622 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OV1-9 R/B
1 02622U 66111D 25309.47813349 .00001115 00000-0 44042-3 0 9990
2 02622 99.0890 323.7157 2223119 48.5335 328.6350 10.49446766221420Epoch: 2025-11-05T11:28Z
TLE epoch observation values (Epoch: 2025-11-05T11:28:30.733Z)
Latitude
-0.00001°
Longitude
106.63742°
Altitude
923.875 km
Speed
7.999 km/s
True Right ascension
21h 34m 51s
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
14:06:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,390.34 km
Perigee altitude
473.237 km
Semi-major axis
8,809.926 km
Eccentricity
0.22231
Inclination
99.089°
RAAN
323.7157°
Arg. of periapsis
48.5335°
True anomaly
311.57998°
Mean anomaly
328.635°
Eccentric anomaly
320.53975°
Mean motion
2.62473 °/min
Orbital period
137.16 mins
BSTAR
0.00044042
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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.OV1-9 R/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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-07 00:13:01.171Z | 115.591° SE | 2025-11-07 00:15:01.171Z | 74.206° E | 19.684° | 2025-11-07 00:17:01.171Z | 26.625° NE |
| 19 mins | 2025-11-07 12:04:01.171Z | 52.428° ENE | 2025-11-07 12:11:01.171Z | 101.617° ESE | 24.892° | 2025-11-07 12:23:01.171Z | 150.25° SSE |
| 23 mins | 2025-11-07 14:18:01.171Z | 7.016° NNE | 2025-11-07 14:25:01.171Z | 285.564° WNW | 43.795° | 2025-11-07 14:41:01.171Z | 206.915° SW |
| 7 mins | 2025-11-07 16:37:01.171Z | 317.588° NNW | 2025-11-07 16:40:01.171Z | 297.615° NW | 13.632° | 2025-11-07 16:44:01.171Z | 277.081° WNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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