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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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
CONE + CYL, 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 26235.61731355 .00000008 00000-0 13702-5 0 9994
2 01314 90.2454 7.7136 0031915 114.0451 257.4400 12.91806234639730Epoch: 2026-08-23T14:48Z
TLE epoch observation values (Epoch: 2026-08-23T14:48:55.890Z)
Latitude
11.08079°
Longitude
173.52211°
Altitude
1,301.881 km
Speed
7.204 km/s
True Right ascension
00h 30m 39s
True Declination
11° 01' 14"
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
17:51:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,315.977 km
Perigee altitude
1,267.021 km
Semi-major axis
7,669.636 km
Eccentricity
0.00319
Inclination
90.2454°
RAAN
7.7136°
Arg. of periapsis
114.0451°
True anomaly
257.08334°
Mean anomaly
257.44°
Eccentric anomaly
257.26164°
Mean motion
3.23133 °/min
Orbital period
111.41 mins
BSTAR
0.0000013702
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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 | 2026-08-24 07:37:58.903Z | 111.484° ESE | 2026-08-24 07:42:58.903Z | 68.623° E | 19.053° | 2026-08-24 07:46:58.903Z | 33.297° NE |
| 13 mins | 2026-08-24 09:26:58.903Z | 184.546° SSW | 2026-08-24 09:32:58.903Z | 255.968° W | 43.968° | 2026-08-24 09:39:58.903Z | 353.405° N |
| 5 mins | 2026-08-24 19:18:58.903Z | 57.321° ENE | 2026-08-24 19:20:58.903Z | 74.008° E | 13.031° | 2026-08-24 19:23:58.903Z | 98.312° ESE |
| 13 mins | 2026-08-24 21:06:58.903Z | 4.789° NNE | 2026-08-24 21:12:58.903Z | 53.3° ENE | 44.614° | 2026-08-24 21:19:58.903Z | 180.562° SSW |
| 8 mins | 2026-08-24 22:59:58.903Z | 321.802° NNW | 2026-08-24 23:03:58.903Z | 286.284° WNW | 16.863° | 2026-08-24 23:07:58.903Z | 253.575° 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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