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: 12 hours ago
TLE from 12 hours ago
0 OPS 4682 (SNAPSHOT)
1 1314U 65027A 25310.58109117 .00000026 00000-0 70175-4 0 9994
2 1314 90.2409 1.3998 0031236 148.6556 7.8111 12.91799684602287Epoch: 2025-11-06T13:56Z
TLE epoch observation values (Epoch: 2025-11-06T13:56:46.277Z)
Latitude
23.50251°
Longitude
-73.72614°
Altitude
1,273.47 km
Speed
7.232 km/s
True Right ascension
12h 06m 00s
True Declination
23° 23' 08"
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
22:07:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,315.482 km
Perigee altitude
1,267.568 km
Semi-major axis
7,669.662 km
Eccentricity
0.00312
Inclination
90.2409°
RAAN
1.3998°
Arg. of periapsis
148.6556°
True anomaly
7.85994°
Mean anomaly
7.8111°
Eccentric anomaly
7.8355°
Mean motion
3.23131 °/min
Orbital period
111.41 mins
BSTAR
0.000070175
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-07 02:18:10.580Z | 109.568° ESE | 2025-11-07 02:22:10.580Z | 75.417° E | 19.423° | 2025-11-07 02:27:10.580Z | 31.01° NE |
| 13 mins | 2025-11-07 04:07:10.580Z | 185.677° SSW | 2025-11-07 04:13:10.580Z | 279.726° WNW | 43.861° | 2025-11-07 04:20:10.580Z | 353.521° N |
| 5 mins | 2025-11-07 13:59:10.580Z | 59.399° ENE | 2025-11-07 14:01:10.580Z | 76.336° E | 13.232° | 2025-11-07 14:04:10.580Z | 100.5° ESE |
| 13 mins | 2025-11-07 15:47:10.580Z | 4.624° NNE | 2025-11-07 15:53:10.580Z | 86.18° E | 44.832° | 2025-11-07 16:00:10.580Z | 181.326° SSW |
| 7 mins | 2025-11-07 17:40:10.580Z | 319.636° NNW | 2025-11-07 17:43:10.580Z | 293.31° NW | 16.657° | 2025-11-07 17:47:10.580Z | 258.698° W |
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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