OV1-14, 3174
Orbit data source: Space-Track
OV1-14, 3174 is a payload satellite owned by USAF OAR (US) that was launched on Sat, 06 Apr 1968 UTC via an ATLAS F 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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3174 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
101 kg wet, 101 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: 10 hours ago
TLE from 10 hours ago
0 OV1-14
1 3174U 68026B 25312.46743050 .00000052 00000-0 85260-4 0 9991
2 3174 100.0041 292.5838 4004770 105.0425 10.0046 6.96697388460945Epoch: 2025-11-08T11:13Z
TLE epoch observation values (Epoch: 2025-11-08T11:13:05.995Z)
Latitude
48.99052°
Longitude
-91.95052°
Altitude
761.88 km
Speed
8.799 km/s
True Right ascension
08h 16m 53s
True Declination
48° 49' 13"
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
17:25:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,836.143 km
Perigee altitude
562.951 km
Semi-major axis
11,577.684 km
Eccentricity
0.40048
Inclination
100.0041°
RAAN
292.5838°
Arg. of periapsis
105.0425°
True anomaly
25.04231°
Mean anomaly
10.0046°
Eccentric anomaly
16.53492°
Mean motion
1.74225 °/min
Orbital period
206.63 mins
BSTAR
0.00008526
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Other satellites on launch #26 in the year 1968 (1968-04-06 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.OV1-14 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 | 2025-11-08 21:13:03.071Z | 61.123° ENE | 2025-11-08 21:13:03.071Z | 61.123° ENE | 26.719° | 2025-11-08 21:17:03.071Z | 17.922° NNE |
| 21 mins | 2025-11-09 00:20:03.071Z | 202.454° SSW | 2025-11-09 00:34:03.071Z | 249.477° W | 24.26° | 2025-11-09 00:41:03.071Z | 305.168° NW |
| 11 mins | 2025-11-09 11:20:03.071Z | 36.351° NE | 2025-11-09 11:23:03.071Z | 117.378° SE | 39.099° | 2025-11-09 11:31:03.071Z | 183.764° SSW |
| 6 mins | 2025-11-09 21:07:03.071Z | 128.787° SE | 2025-11-09 21:13:03.071Z | 116.095° SE | 21.64° | 2025-11-09 21:13:03.071Z | 116.095° SE |
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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