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: 10 hours ago
TLE from 10 hours ago
0 OV1-14
1 03174U 68026B 25342.46669991 .00000262 00000-0 44965-3 0 9994
2 03174 100.0113 301.7020 4001797 82.6761 12.0956 6.96707946463037Epoch: 2025-12-08T11:12Z
TLE epoch observation values (Epoch: 2025-12-08T11:12:02.872Z)
Latitude
65.39744°
Longitude
-101.23163°
Altitude
853.946 km
Speed
8.721 km/s
True Right ascension
09h 36m 58s
True Declination
65° 16' 07"
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
19:00:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,832.539 km
Perigee altitude
566.323 km
Semi-major axis
11,577.568 km
Eccentricity
0.40018
Inclination
100.0113°
RAAN
301.702°
Arg. of periapsis
82.6761°
True anomaly
30.00839°
Mean anomaly
12.0956°
Eccentric anomaly
19.90005°
Mean motion
1.74228 °/min
Orbital period
206.63 mins
BSTAR
0.00044965
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-12-08 21:05:25.126Z | 159.362° S | 2025-12-08 21:15:25.126Z | 64.548° ENE | 44.646° | 2025-12-08 21:19:25.126Z | 348.301° N |
| 8 mins | 2025-12-09 08:01:25.126Z | 91.225° ESE | 2025-12-09 08:04:25.126Z | 109.076° ESE | 13.175° | 2025-12-09 08:09:25.126Z | 129.839° SE |
| 17 mins | 2025-12-09 11:21:25.126Z | 348.151° N | 2025-12-09 11:25:25.126Z | 288.409° WNW | 34.951° | 2025-12-09 11:38:25.126Z | 220.52° SW |
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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