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
Defense Technology
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
Cone + Cyl, Unknown HBR
Radar Cross Section
14.538 m², 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 25259.27557384 .00000042 00000-0 13139-3 0 9999
2 01314 90.2452 0.2672 0028616 285.9559 89.2294 12.91798224595666Epoch: 2025-09-16T06:36Z
TLE epoch observation values (Epoch: 2025-09-16T06:36:49.579Z)
Latitude
15.49014°
Longitude
-94.4752°
Altitude
1,296.356 km
Speed
7.209 km/s
True Right ascension
00h 00m 47s
True Declination
15° 24' 29"
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
11:28:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,313.478 km
Perigee altitude
1,269.583 km
Semi-major axis
7,669.668 km
Eccentricity
0.00286
Inclination
90.2452°
RAAN
0.2672°
Arg. of periapsis
285.9559°
True anomaly
89.5573°
Mean anomaly
89.2294°
Eccentric anomaly
89.39335°
Mean motion
3.23131 °/min
Orbital period
111.41 mins
BSTAR
0.00013139
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-09-16 20:09:15.839Z | 345.791° N | 2025-09-16 20:16:15.839Z | 275.702° WNW | 31.804° | 2025-09-16 20:22:15.839Z | 220.51° SW |
| 13 mins | 2025-09-17 06:48:15.839Z | 161.513° S | 2025-09-17 06:54:15.839Z | 92.511° ESE | 42.723° | 2025-09-17 07:01:15.839Z | 3.888° NNE |
| 9 mins | 2025-09-17 08:42:15.839Z | 243.699° WSW | 2025-09-17 08:46:15.839Z | 281.411° WNW | 20.958° | 2025-09-17 08:51:15.839Z | 325.781° NNW |
| 13 mins | 2025-09-17 18:28:15.839Z | 15.479° NNE | 2025-09-17 18:35:15.839Z | 99.041° ESE | 37.396° | 2025-09-17 18:41:15.839Z | 158.907° S |
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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