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: 8 hours ago
TLE from 8 hours ago
0 OV1-14
1 03174U 68026B 25292.22615708 .00000183 00000-0 30068-3 0 9990
2 03174 100.0022 286.4280 4006891 120.1242 2.7524 6.96692850459539Epoch: 2025-10-19T05:25Z
TLE epoch observation values (Epoch: 2025-10-19T05:25:39.971Z)
Latitude
51.83765°
Longitude
9.95833°
Altitude
583.243 km
Speed
8.961 km/s
True Right ascension
07h 57m 16s
True Declination
51° 39' 58"
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
08:34:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,838.668 km
Perigee altitude
560.525 km
Semi-major axis
11,577.733 km
Eccentricity
0.40069
Inclination
100.0022°
RAAN
286.428°
Arg. of periapsis
120.1242°
True anomaly
7.01106°
Mean anomaly
2.7524°
Eccentric anomaly
4.58933°
Mean motion
1.74224 °/min
Orbital period
206.63 mins
BSTAR
0.00030068
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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. |
|---|---|---|---|---|---|---|---|
| 27 mins | 2025-10-19 21:57:41.115Z | 131.775° SE | 2025-10-19 22:17:41.115Z | 66.662° ENE | 34.668° | 2025-10-19 22:24:41.115Z | 4.679° NNE |
| 31 mins | 2025-10-20 01:16:41.115Z | 199.725° SSW | 2025-10-20 01:38:41.115Z | 254.869° W | 27.272° | 2025-10-20 01:47:41.115Z | 310.855° NW |
| 8 mins | 2025-10-20 12:26:41.115Z | 28.165° NE | 2025-10-20 12:28:41.115Z | 73.283° E | 40.242° | 2025-10-20 12:34:41.115Z | 187.064° SSW |
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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