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: 15 hours ago
TLE from 15 hours ago
0 OV1-14
1 3174U 68026B 25289.06171149 .00000014 00000-0 21420-4 0 9990
2 3174 100.0022 285.4652 4007159 122.4810 346.0346 6.96692335459315Epoch: 2025-10-16T01:28Z
TLE epoch observation values (Epoch: 2025-10-16T01:28:51.872Z)
Latitude
79.86859°
Longitude
159.44126°
Altitude
939.178 km
Speed
8.649 km/s
True Right ascension
13h 45m 56s
True Declination
79° 48' 37"
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
11:29:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,838.986 km
Perigee altitude
560.218 km
Semi-major axis
11,577.739 km
Eccentricity
0.40072
Inclination
100.0022°
RAAN
285.4652°
Arg. of periapsis
122.481°
True anomaly
325.59058°
Mean anomaly
346.0346°
Eccentric anomaly
337.10091°
Mean motion
1.74224 °/min
Orbital period
206.63 mins
BSTAR
0.00002142
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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. |
|---|---|---|---|---|---|---|---|
| 24 mins | 2025-10-16 21:39:43.657Z | 120.548° SE | 2025-10-16 21:55:43.657Z | 73.611° E | 28.797° | 2025-10-16 22:03:43.657Z | 10.445° NNE |
| 36 mins | 2025-10-17 00:51:43.657Z | 187.615° SSW | 2025-10-17 01:18:43.657Z | 256.168° W | 33.896° | 2025-10-17 01:27:43.657Z | 320.406° NNW |
| 6 mins | 2025-10-17 12:06:43.657Z | 59.267° ENE | 2025-10-17 12:08:43.657Z | 111.423° ESE | 26.754° | 2025-10-17 12:12:43.657Z | 165.486° S |
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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