OV1-5, 2122
Orbit data source: Space-Track
OV1-5, 2122 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Wed, 30 Mar 1966 UTC via an ATLAS D launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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2122 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
OV1, Unknown motor
Mass
114 kg wet, 114 kg dry
Launch date (UTC)
Launch vehicle
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: 9 hours ago
TLE from 9 hours ago
0 OV1-5
1 2122U 66025B 26035.40384353 .00000342 00000-0 99653-4 0 9997
2 2122 144.6377 16.9489 0046703 75.5954 284.9896 13.66154492986946Epoch: 2026-02-04T09:41Z
TLE epoch observation values (Epoch: 2026-02-04T09:41:32.080Z)
Latitude
-0.00005°
Longitude
96.99439°
Altitude
1,003.652 km
Speed
7.356 km/s
True Right ascension
01h 07m 47s
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
21:07:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,050.914 km
Perigee altitude
981.845 km
Semi-major axis
7,394.517 km
Eccentricity
0.00467
Inclination
144.6377°
RAAN
16.9489°
Arg. of periapsis
75.5954°
True anomaly
284.47186°
Mean anomaly
284.9896°
Eccentric anomaly
284.73081°
Mean motion
3.41333 °/min
Orbital period
105.47 mins
BSTAR
0.000099653
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Other satellites on launch #25 in the year 1966 (1966-03-30 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.OV1-5 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-04 20:24:52.722Z | 156.441° SSE | 2026-02-04 20:28:52.722Z | 207.117° SW | 23.301° | 2026-02-04 20:32:52.722Z | 255.367° W |
| 7 mins | 2026-02-05 14:18:52.722Z | 113.147° SE | 2026-02-05 14:21:52.722Z | 154.383° SSE | 24.257° | 2026-02-05 14:25:52.722Z | 205.538° SW |
| 9 mins | 2026-02-05 15:57:52.722Z | 100.402° ESE | 2026-02-05 16:01:52.722Z | 167.177° S | 37.045° | 2026-02-05 16:06:52.722Z | 240.102° WSW |
| 9 mins | 2026-02-05 17:37:52.722Z | 108.696° ESE | 2026-02-05 17:41:52.722Z | 190.822° SSW | 40.416° | 2026-02-05 17:46:52.722Z | 259.353° W |
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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