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 01314U 65027A 25340.62482021 .00000038 00000-0 11176-3 0 9998
2 01314 90.2365 2.0464 0031946 74.0505 41.8606 12.91800755606168Epoch: 2025-12-06T14:59Z
TLE epoch observation values (Epoch: 2025-12-06T14:59:44.466Z)
Latitude
63.92441°
Longitude
-118.05789°
Altitude
1,287.24 km
Speed
7.227 km/s
True Right ascension
12h 10m 06s
True Declination
63° 47' 52"
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
00:56:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,316.022 km
Perigee altitude
1,267.019 km
Semi-major axis
7,669.658 km
Eccentricity
0.00319
Inclination
90.2365°
RAAN
2.0464°
Arg. of periapsis
74.0505°
True anomaly
42.10562°
Mean anomaly
41.8606°
Eccentric anomaly
41.98304°
Mean motion
3.23131 °/min
Orbital period
111.41 mins
BSTAR
0.00011176
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-07 03:32:18.865Z | 237.412° WSW | 2025-12-07 03:37:18.865Z | 280.882° WNW | 19.754° | 2025-12-07 03:42:18.865Z | 325.197° NNW |
| 13 mins | 2025-12-07 13:19:18.865Z | 15.431° NNE | 2025-12-07 13:25:18.865Z | 81.123° E | 38.086° | 2025-12-07 13:32:18.865Z | 161.088° S |
| 11 mins | 2025-12-07 15:11:18.865Z | 335.622° NNW | 2025-12-07 15:16:18.865Z | 286.115° WNW | 26.375° | 2025-12-07 15:22:18.865Z | 230.833° WSW |
| 5 mins | 2025-12-08 00:03:18.865Z | 85.242° E | 2025-12-08 00:05:18.865Z | 68.136° E | 14.214° | 2025-12-08 00:08:18.865Z | 42.986° NE |
| 13 mins | 2025-12-08 01:49:18.865Z | 172.542° S | 2025-12-08 01:55:18.865Z | 111.218° ESE | 44.873° | 2025-12-08 02:02:18.865Z | 358.876° 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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