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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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: 6 days ago
TLE from 6 days ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 26155.12590838 .00000122 00000-0 22018-3 0 9999
2 01514 89.9973 227.8998 0069728 195.7088 225.0994 13.35368135959522Epoch: 2026-06-04T03:01Z
TLE epoch observation values (Epoch: 2026-06-04T03:01:18.484Z)
Latitude
60.33388°
Longitude
-69.99716°
Altitude
1,174.062 km
Speed
7.254 km/s
True Right ascension
15h 11m 37s
True Declination
60° 11' 38"
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
09:35:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,175.963 km
Perigee altitude
1,071.346 km
Semi-major axis
7,501.791 km
Eccentricity
0.00697
Inclination
89.9973°
RAAN
227.8998°
Arg. of periapsis
195.7088°
True anomaly
224.5369°
Mean anomaly
225.0994°
Eccentric anomaly
224.8178°
Mean motion
3.34038 °/min
Orbital period
107.77 mins
BSTAR
0.00022018
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-06-10 04:28:42.736Z | 161.04° S | 2026-06-10 04:34:42.736Z | 99.935° ESE | 41.517° | 2026-06-10 04:41:42.736Z | 4.959° NNE |
| 8 mins | 2026-06-10 06:19:42.736Z | 244.353° WSW | 2026-06-10 06:22:42.736Z | 274.762° WNW | 20.566° | 2026-06-10 06:27:42.736Z | 324.536° NNW |
| 10 mins | 2026-06-10 15:47:42.736Z | 29.901° NE | 2026-06-10 15:52:42.736Z | 89.97° E | 26.558° | 2026-06-10 15:57:42.736Z | 141.127° SSE |
| 10 mins | 2026-06-10 17:35:42.736Z | 340.016° N | 2026-06-10 17:39:42.736Z | 286.771° WNW | 33.873° | 2026-06-10 17:45:42.736Z | 213.859° SW |
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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