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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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
DOMED CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OV1-14
1 03174U 68026B 26305.10897321 -.00000206 00000-0 -30080-3 0 9998
2 03174 100.0105 41.3992 4016379 198.4330 322.9263 6.96785827485855Epoch: 2026-11-01T02:36Z
TLE epoch observation values (Epoch: 2026-11-01T02:36:55.285Z)
Latitude
58.66362°
Longitude
158.5396°
Altitude
2,622.816 km
Speed
7.367 km/s
True Right ascension
15h 52m 42s
True Declination
58° 32' 33"
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
23:11:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,848.205 km
Perigee altitude
548.922 km
Semi-major axis
11,576.7 km
Eccentricity
0.40164
Inclination
100.0105°
RAAN
41.3992°
Arg. of periapsis
198.433°
True anomaly
281.49293°
Mean anomaly
322.9263°
Eccentric anomaly
303.80458°
Mean motion
1.74247 °/min
Orbital period
206.6 mins
BSTAR
-0.0003008
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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. |
|---|---|---|---|---|---|---|---|
| 91 mins | 2026-11-03 04:30:21.180Z | 132.138° SE | 2026-11-03 05:28:21.180Z | 58.52° ENE | 72.031° | 2026-11-03 06:01:21.180Z | 347.595° N |
| 97 mins | 2026-11-03 07:46:21.180Z | 191.576° SSW | 2026-11-03 08:39:21.180Z | 260.415° W | 47.314° | 2026-11-03 09:23:21.180Z | 339.96° N |
| 21 mins | 2026-11-03 19:54:21.180Z | 11.946° NNE | 2026-11-03 20:09:21.180Z | 308.2° NW | 58.058° | 2026-11-03 20:15:21.180Z | 222.581° SW |
| 18 mins | 2026-11-03 23:11:21.180Z | 18.376° NNE | 2026-11-03 23:21:21.180Z | 355.391° N | 15.549° | 2026-11-03 23:29:21.180Z | 324.773° NNW |
| 51 mins | 2026-11-04 01:54:21.180Z | 75.092° E | 2026-11-04 02:26:21.180Z | 35.606° NE | 29.024° | 2026-11-04 02:45:21.180Z | 350.276° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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