OPS 4682 (SNAPSHOT), 1314
Orbit data source: Space-Track
OPS 4682 (SNAPSHOT), 1314 is an American payload satellite in LEO that was launched on Sat, 03 Apr 1965 UTC via an ATLAS SLV-3 AGENA D 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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1314 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
SNAP 10 REACTOR, Unknown motor
Mass
2,386 kg wet, 422 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 2.3 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 OPS 4682 (SNAPSHOT)
1 01314U 65027A 25292.69150545 .00000048 00000-0 15099-3 0 9993
2 01314 90.2438 1.0079 0029888 194.8234 333.1712 12.91799047599978Epoch: 2025-10-19T16:35Z
TLE epoch observation values (Epoch: 2025-10-19T16:35:46.070Z)
Latitude
12.11884°
Longitude
-96.2865°
Altitude
1,276.056 km
Speed
7.228 km/s
True Right ascension
12h 04m 14s
True Declination
12° 03' 12"
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
05:55:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,314.451 km
Perigee altitude
1,268.604 km
Semi-major axis
7,669.664 km
Eccentricity
0.00299
Inclination
90.2438°
RAAN
1.0079°
Arg. of periapsis
194.8234°
True anomaly
333.01611°
Mean anomaly
333.1712°
Eccentric anomaly
333.09371°
Mean motion
3.23131 °/min
Orbital period
111.41 mins
BSTAR
0.00015099
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Other satellites on launch #27 in the year 1965 (1965-04-03 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.OPS 4682 (SNAPSHOT) 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 | 2025-10-20 16:30:34.881Z | 12.285° NNE | 2025-10-20 16:37:34.881Z | 100.768° ESE | 40.011° | 2025-10-20 16:44:34.881Z | 166.776° S |
| 10 mins | 2025-10-20 18:23:34.881Z | 329.579° NNW | 2025-10-20 18:27:34.881Z | 290.131° WNW | 24.086° | 2025-10-20 18:33:34.881Z | 235.405° WSW |
| 7 mins | 2025-10-21 03:13:34.881Z | 95.256° ESE | 2025-10-21 03:16:34.881Z | 69.527° E | 16.566° | 2025-10-21 03:20:34.881Z | 36.072° NE |
| 14 mins | 2025-10-21 05:00:34.881Z | 177.189° S | 2025-10-21 05:06:34.881Z | 208.915° SW | 44.868° | 2025-10-21 05:14:34.881Z | 357.059° N |
| 6 mins | 2025-10-21 06:56:34.881Z | 264.496° W | 2025-10-21 06:58:34.881Z | 281.082° WNW | 14.498° | 2025-10-21 07:02:34.881Z | 313.835° 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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