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: 9 hours ago
TLE from 9 hours ago
0 OV1-14
1 3174U 68026B 26036.73847451 .00000422 00000-0 70833-3 0 9995
2 3174 100.0211 319.7355 4005492 38.4742 356.7940 6.96732252467167Epoch: 2026-02-05T17:43Z
TLE epoch observation values (Epoch: 2026-02-05T17:43:24.197Z)
Latitude
29.86482°
Longitude
-87.79154°
Altitude
585.318 km
Speed
8.954 km/s
True Right ascension
20h 55m 46s
True Declination
29° 42' 46"
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
04:22:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,836.438 km
Perigee altitude
561.883 km
Semi-major axis
11,577.298 km
Eccentricity
0.40055
Inclination
100.0211°
RAAN
319.7355°
Arg. of periapsis
38.4742°
True anomaly
351.8409°
Mean anomaly
356.794°
Eccentric anomaly
354.65694°
Mean motion
1.74234 °/min
Orbital period
206.62 mins
BSTAR
0.00070833
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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. |
|---|---|---|---|---|---|---|---|
| 43 mins | 2026-02-06 04:30:39.578Z | 52.884° ENE | 2026-02-06 04:45:39.578Z | 100.309° ESE | 20.535° | 2026-02-06 05:13:39.578Z | 144.201° SSE |
| 51 mins | 2026-02-06 07:51:39.578Z | 12.395° NNE | 2026-02-06 08:02:39.578Z | 301.795° NW | 44.774° | 2026-02-06 08:42:39.578Z | 209.335° SW |
| 12 mins | 2026-02-06 11:19:39.578Z | 326.522° NNW | 2026-02-06 11:23:39.578Z | 308.713° NW | 14.071° | 2026-02-06 11:31:39.578Z | 285.346° WNW |
| 5 mins | 2026-02-06 17:51:39.578Z | 108.472° ESE | 2026-02-06 17:53:39.578Z | 56.471° ENE | 23.528° | 2026-02-06 17:56:39.578Z | 6.498° 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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