OPS 8464 (TRANSIT 5B-7), 1514
Orbit data source: Space-Track
OPS 8464 (TRANSIT 5B-7), 1514 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Fri, 13 Aug 1965 UTC via a THOR ABLESTAR 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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1514 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NAFI
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~54 kg wet, ~54 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 25296.55558721 .00000127 00000-0 22898-3 0 9997
2 01514 89.9830 228.1306 0071909 106.5484 66.5261 13.35322427929688Epoch: 2025-10-23T13:20Z
TLE epoch observation values (Epoch: 2025-10-23T13:20:02.734Z)
Latitude
6.08893°
Longitude
175.90425°
Altitude
1,107.931 km
Speed
7.309 km/s
True Right ascension
03h 12m 30s
True Declination
6° 03' 16"
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
15:23:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,177.771 km
Perigee altitude
1,069.88 km
Semi-major axis
7,501.962 km
Eccentricity
0.00719
Inclination
89.983°
RAAN
228.1306°
Arg. of periapsis
106.5484°
True anomaly
67.28462°
Mean anomaly
66.5261°
Eccentric anomaly
66.90509°
Mean motion
3.34026 °/min
Orbital period
107.78 mins
BSTAR
0.00022898
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Other satellites on launch #65 in the year 1965 (1965-08-13 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 8464 (TRANSIT 5B-7) 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-23 21:37:02.414Z | 250.977° W | 2025-10-23 21:40:02.414Z | 279.639° WNW | 16.118° | 2025-10-23 21:44:02.414Z | 317.901° NNW |
| 11 mins | 2025-10-24 07:04:02.414Z | 24.124° NE | 2025-10-24 07:09:02.414Z | 85.865° E | 30.965° | 2025-10-24 07:15:02.414Z | 150.569° SSE |
| 10 mins | 2025-10-24 08:52:02.414Z | 337.379° NNW | 2025-10-24 08:56:02.414Z | 290.855° WNW | 29.404° | 2025-10-24 09:02:02.414Z | 221.526° SW |
| 11 mins | 2025-10-24 19:10:02.414Z | 142.766° SSE | 2025-10-24 19:15:02.414Z | 78.567° E | 34.165° | 2025-10-24 19:21:02.414Z | 12.235° NNE |
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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