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
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 26078.56682876 .00000392 00000-0 62763-3 0 9999
2 03174 100.0102 332.4810 4012528 7.3565 153.4538 6.96749804470070Epoch: 2026-03-19T13:36Z
TLE epoch observation values (Epoch: 2026-03-19T13:36:14.004Z)
Latitude
5.02583°
Longitude
132.19561°
Altitude
9,595.415 km
Speed
3.936 km/s
True Right ascension
10h 13m 28s
True Declination
5° 00' 45"
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
14:26:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,844.308 km
Perigee altitude
553.62 km
Semi-major axis
11,577.101 km
Eccentricity
0.40125
Inclination
100.0102°
RAAN
332.481°
Arg. of periapsis
7.3565°
True anomaly
167.48515°
Mean anomaly
153.4538°
Eccentric anomaly
160.95552°
Mean motion
1.74238 °/min
Orbital period
206.61 mins
BSTAR
0.00062763
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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. |
|---|---|---|---|---|---|---|---|
| 18 mins | 2026-03-20 09:35:13.271Z | 297.507° NW | 2026-03-20 09:35:13.271Z | 297.507° NW | 22.187° | 2026-03-20 09:53:13.271Z | 275.771° WNW |
| 10 mins | 2026-03-20 15:48:13.271Z | 106.774° ESE | 2026-03-20 15:51:13.271Z | 46.655° ENE | 29.802° | 2026-03-20 15:58:13.271Z | 354.516° N |
| 79 mins | 2026-03-21 02:36:13.271Z | 33.959° NE | 2026-03-21 03:05:13.271Z | 98.478° ESE | 29.939° | 2026-03-21 03:55:13.271Z | 159.067° S |
| 78 mins | 2026-03-21 05:57:13.271Z | 12.545° NNE | 2026-03-21 06:19:13.271Z | 295.31° NW | 44.556° | 2026-03-21 07:15:13.271Z | 217.635° SW |
| 13 mins | 2026-03-21 09:22:13.271Z | 354.865° N | 2026-03-21 09:34:13.271Z | 316.289° NNW | 22.956° | 2026-03-21 09:35:13.271Z | 313.656° NW |
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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