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OV1-2, 1613

Orbit data source: Space-Track

OV1-2, 1613 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Tue, 05 Oct 1965 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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Identifier
1613, 1965-078A
Orbit
LEO
Last TLE update
14 hours ago
Origin
Manufacturer
GD/Convair
Mission
Civil Science
Bus & Motor
OV1, Unknown motor
Mass
86 kg wet, 86 kg dry
Launch date (UTC)
1965-10-05 (60 years ago)
Launch vehicle
ATLAS D
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Domed Cyl, 1.4 m
Radar Cross Section
0.946 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 14 hours ago
0 OV1-2
1 01613U 65078A   25129.27259389  .00008435  00000-0  83727-3 0  9991
2 01613 144.2295  35.1138 1146779   3.8660 357.0209 12.96890590662176
Epoch: 2025-05-09T06:32Z
Definitive object data (Epoch: 2025-05-09T06:32:32.112Z)
Latitude
0.00001°
Longitude
69.64888°
Altitude
397.49 km
Speed
8.1 km/s
True Right ascension
02h 20m 27s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
-35.89525°
Longitude
163.89568°
Altitude
1,319.686 km
Speed
7.181 km/s
Apparent Right ascension
11h 57m 17s
Apparent Declination
-59° 15' 44"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
05:06:29
Azimuth
139.662° SSE
Elevation
-39.62°
Doppler factor
1
Orbital elements
Apogee altitude
2,155.059 km
Perigee altitude
399.271 km
Semi-major axis
7,655.302 km
Eccentricity
0.1146779
Inclination
144.2295°
RAAN
35.1138°
Arg. of periapsis
3.866°
True anomaly
356.22477°
Mean anomaly
357.0209°
Eccentric anomaly
356.63526°
Mean motion
3.24041 °/min
BSTAR
0.00083727
Orbital period
111.1 mins
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Other satellites on launch #78 in the year 1965 (1965-10-05 UTC)

OV1-2 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.
11 mins2025-05-10 07:11:16.916Z111.958° ESE2025-05-10 07:17:16.916Z152.275° SSE16.677°2025-05-10 07:22:16.916Z181.745° SSW
14 mins2025-05-10 08:55:16.916Z100.851° ESE2025-05-10 09:01:16.916Z162.683° S30.113°2025-05-10 09:09:16.916Z218.522° SW
12 mins2025-05-10 10:41:16.916Z100.535° ESE2025-05-10 10:45:16.916Z166.356° S39.221°2025-05-10 10:53:16.916Z243.842° WSW
10 mins2025-05-10 12:27:16.916Z110.096° ESE2025-05-10 12:30:16.916Z184.521° SSW41.392°2025-05-10 12:37:16.916Z262.491° W
7 mins2025-05-10 14:13:16.916Z140.761° SSE2025-05-10 14:15:16.916Z185.231° SSW31.816°2025-05-10 14:20:16.916Z265.12° W
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