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
Country
USRelated business
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
Shape & HBR
Box + 4 Pan, 1.3 m
Radar Cross Section
1.167 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OV2-5
1 03428U 68081A 25241.96844867 -.00000215 00000-0 00000-0 0 9995
2 03428 1.4417 39.0608 0079135 288.8797 64.4680 1.01561729118095Epoch: 2025-08-29T23:14Z
TLE epoch observation values (Epoch: 2025-08-29T23:14:33.965Z)
Latitude
-0.16367°
Longitude
66.17878°
Altitude
35,286.915 km
Speed
3.098 km/s
True Right ascension
02h 12m 55s
True Declination
0° 09' 49"
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
17:20:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,760.736 km
Perigee altitude
35,099.04 km
Semi-major axis
41,808.025 km
Eccentricity
0.00791
Inclination
1.4417°
RAAN
39.0608°
Arg. of periapsis
288.8797°
True anomaly
65.28974°
Mean anomaly
64.468°
Eccentric anomaly
64.87852°
Mean motion
0.25389 °/min
Orbital period
1,417.91 mins
BSTAR
0
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Other satellites on launch #81 in the year 1968 (1968-09-26 UTC)
OV2-5 Visibility
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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3428 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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