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: 21 hours ago
TLE from 21 hours ago
0 OV1-14
1 3174U 68026B 26307.09683005 -.00000271 00000-0 -39874-3 0 9992
2 3174 100.0107 42.0057 4016389 196.9589 269.3196 6.96785146485995Epoch: 2026-11-03T02:19Z
TLE epoch observation values (Epoch: 2026-11-03T02:19:26.116Z)
Latitude
62.79195°
Longitude
-55.23884°
Altitude
6,954.469 km
Speed
5.043 km/s
True Right ascension
01h 27m 56s
True Declination
62° 43' 01"
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
19:21:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,848.227 km
Perigee altitude
548.915 km
Semi-major axis
11,576.708 km
Eccentricity
0.40164
Inclination
100.0107°
RAAN
42.0057°
Arg. of periapsis
196.9589°
True anomaly
227.55522°
Mean anomaly
269.3196°
Eccentric anomaly
247.98526°
Mean motion
1.74247 °/min
Orbital period
206.6 mins
BSTAR
-0.00039874
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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. |
|---|---|---|---|---|---|---|---|
| 53 mins | 2026-11-04 01:52:29.523Z | 76.278° E | 2026-11-04 02:26:29.523Z | 35.303° NE | 29.029° | 2026-11-04 02:45:29.523Z | 349.948° N |
| 91 mins | 2026-11-04 04:37:29.523Z | 134.788° SE | 2026-11-04 05:34:29.523Z | 62.226° ENE | 74.851° | 2026-11-04 06:08:29.523Z | 347.286° N |
| 95 mins | 2026-11-04 07:54:29.523Z | 195.11° SSW | 2026-11-04 08:46:29.523Z | 261.889° W | 44.478° | 2026-11-04 09:29:29.523Z | 338.421° N |
| 20 mins | 2026-11-04 20:01:29.523Z | 11.357° NNE | 2026-11-04 20:16:29.523Z | 296.812° NW | 52.102° | 2026-11-04 20:21:29.523Z | 230.679° WSW |
| 12 mins | 2026-11-04 23:17:29.523Z | 19.919° NNE | 2026-11-04 23:27:29.523Z | 357.319° N | 15.076° | 2026-11-04 23:29:29.523Z | 350.87° 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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