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: 20 hours ago
TLE from 20 hours ago
0 OV1-14
1 03174U 68026B 26037.04020479 .00000391 00000-0 65739-3 0 9997
2 03174 100.0210 319.8273 4005544 38.2493 33.6049 6.96732319467182Epoch: 2026-02-06T00:57Z
TLE epoch observation values (Epoch: 2026-02-06T00:57:53.693Z)
Latitude
66.75503°
Longitude
13.34423°
Altitude
2,330.362 km
Speed
7.569 km/s
True Right ascension
10h 56m 00s
True Declination
66° 39' 10"
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
23:17:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,836.497 km
Perigee altitude
561.823 km
Semi-major axis
11,577.297 km
Eccentricity
0.40055
Inclination
100.021°
RAAN
319.8273°
Arg. of periapsis
38.2493°
True anomaly
72.90797°
Mean anomaly
33.6049°
Eccentric anomaly
51.58765°
Mean motion
1.74234 °/min
Orbital period
206.62 mins
BSTAR
0.00065739
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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. |
|---|---|---|---|---|---|---|---|
| 46 mins | 2026-02-07 04:37:09.971Z | 50.893° ENE | 2026-02-07 04:52:09.971Z | 100.486° ESE | 22.718° | 2026-02-07 05:23:09.971Z | 148.881° SSE |
| 51 mins | 2026-02-07 07:58:09.971Z | 10.735° NNE | 2026-02-07 08:10:09.971Z | 281.099° WNW | 44.413° | 2026-02-07 08:49:09.971Z | 212.178° SW |
| 9 mins | 2026-02-07 11:27:09.971Z | 323.573° NNW | 2026-02-07 11:30:09.971Z | 310.812° NW | 12.66° | 2026-02-07 11:36:09.971Z | 292.221° WNW |
| 5 mins | 2026-02-07 17:58:09.971Z | 120.609° SE | 2026-02-07 18:00:09.971Z | 65.116° ENE | 28.512° | 2026-02-07 18:03:09.971Z | 4.708° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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