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
Civil Science
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, 0.7 m
Radar Cross Section
0.946 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OV1-14
1 03174U 68026B 25258.78579503 .00000170 00000-0 27795-3 0 9994
2 03174 100.0056 276.2460 4009039 145.0174 11.6116 6.96684839457206Epoch: 2025-09-15T18:51Z
TLE epoch observation values (Epoch: 2025-09-15T18:51:32.69Z)
Latitude
5.89417°
Longitude
179.41214°
Altitude
816.81 km
Speed
8.742 km/s
True Right ascension
06h 29m 08s
True Declination
5° 51' 34"
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
12:37:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,841.278 km
Perigee altitude
558.091 km
Semi-major axis
11,577.822 km
Eccentricity
0.4009
Inclination
100.0056°
RAAN
276.246°
Arg. of periapsis
145.0174°
True anomaly
28.921°
Mean anomaly
11.6116°
Eccentric anomaly
19.1448°
Mean motion
1.74222 °/min
Orbital period
206.63 mins
BSTAR
0.00027795
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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. |
|---|---|---|---|---|---|---|---|
| 21 mins | 2025-09-16 21:38:17.034Z | 87.345° E | 2025-09-16 21:51:17.034Z | 55.844° ENE | 18.399° | 2025-09-16 21:59:17.034Z | 18.003° NNE |
| 55 mins | 2025-09-17 00:31:17.034Z | 155.856° SSE | 2025-09-17 01:12:17.034Z | 232.993° WSW | 44.981° | 2025-09-17 01:26:17.034Z | 344.478° N |
| 37 mins | 2025-09-17 04:06:17.034Z | 225.953° WSW | 2025-09-17 04:29:17.034Z | 261.75° W | 17.184° | 2025-09-17 04:43:17.034Z | 300.117° NW |
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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