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: 8 hours ago
TLE from 8 hours ago
0 OV1-14
1 3174U 68026B 26127.59906475 -.00000460 00000-0 -70946-3 0 9991
2 3174 99.9818 347.4073 4012065 330.8659 21.9693 6.96760940473495Epoch: 2026-05-07T14:22Z
TLE epoch observation values (Epoch: 2026-05-07T14:22:39.194Z)
Latitude
22.32752°
Longitude
-97.82261°
Altitude
1,408.333 km
Speed
8.247 km/s
True Right ascension
22h 53m 08s
True Declination
22° 13' 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
06:01:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
9,843.597 km
Perigee altitude
554.081 km
Semi-major axis
11,576.976 km
Eccentricity
0.40121
Inclination
99.9818°
RAAN
347.4073°
Arg. of periapsis
330.8659°
True anomaly
51.8111°
Mean anomaly
21.9693°
Eccentric anomaly
35.22976°
Mean motion
1.74241 °/min
Orbital period
206.61 mins
BSTAR
-0.00070946
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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. |
|---|---|---|---|---|---|---|---|
| 103 mins | 2026-05-08 01:16:49.371Z | 15.329° NNE | 2026-05-08 02:07:49.371Z | 103.943° ESE | 41.025° | 2026-05-08 02:59:49.371Z | 180.542° SSW |
| 91 mins | 2026-05-08 04:39:49.371Z | 12.223° NNE | 2026-05-08 05:15:49.371Z | 308.002° NW | 41.33° | 2026-05-08 06:10:49.371Z | 240.458° WSW |
| 51 mins | 2026-05-08 07:59:49.371Z | 17.015° NNE | 2026-05-08 08:18:49.371Z | 337.03° NNW | 23.731° | 2026-05-08 08:50:49.371Z | 299.27° NW |
| 28 mins | 2026-05-08 11:12:49.371Z | 54.478° ENE | 2026-05-08 11:21:49.371Z | 17.25° NNE | 21.617° | 2026-05-08 11:40:49.371Z | 340.786° N |
| 27 mins | 2026-05-08 14:29:49.371Z | 165.432° S | 2026-05-08 14:34:49.371Z | 199.556° SSW | 44.921° | 2026-05-08 14:56:49.371Z | 346.479° 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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