OV2-5, 3428
Orbit data source: Space-Track
OV2-5, 3428 is a payload satellite owned by SAMSO (US) in GEO that was launched on Thu, 26 Sep 1968 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). 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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3428 intel report (Beta)
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Edit Public Description
Identifier | |
Orbit | GEO |
Last TLE update | 9 hours ago |
Origin | |
Manufacturer | Northrop |
Mission | Non-operational Civil Science |
Bus & Motor | OV2, Unknown motor |
Mass | ~200 kg wet, ~200 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box + 4 Pan, 2.5 m |
Radar Cross Section | 1.167 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 OV2-5
1 03428U 68081A 25093.84312409 -.00000301 00000-0 00000-0 0 9995
2 03428 1.2253 28.3862 0081186 297.7910 268.8765 1.01560769116599
Epoch: 2025-04-03T20:14Z
Definitive object data (Epoch: 2025-04-03T20:14:05.921Z)
Latitude | -0.52573° |
Longitude | 98.19949° |
Altitude | 35,439.253 km |
Speed | 3.087 km/s |
True Right ascension | 15h 36m 32s |
True Declination | 0° 31' 31" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -0.281° |
Longitude | -121.00764° |
Altitude | 35,202.418 km |
Speed | 3.105 km/s |
Apparent Right ascension | 00h 48m 44s |
Apparent Declination | -5° 18' 29" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 11:12:50 |
Azimuth | 321.733° NNW |
Elevation | -49.217° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,769.576 km |
Perigee altitude | 35,090.727 km |
Semi-major axis | 41,808.289 km |
Eccentricity | 0.0081186 |
Inclination | 1.2253° |
RAAN | 28.3862° |
Arg. of periapsis | 297.791° |
True anomaly | 267.94658° |
Mean anomaly | 268.8765° |
Eccentric anomaly | 268.41152° |
Mean motion | 0.25389 °/min |
BSTAR | Unknown |
Orbital period | 1417.92 mins |
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3428 neighbors
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Other satellites on launch #81 in the year 1968 (1968-09-26 UTC)
OV2-5 Visibility forecast
Observer location: undefined°, undefined°
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. |
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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