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: 14 hours ago
TLE from 14 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 25310.76359677 .00000134 00000-0 24143-3 0 9999
2 01514 89.9847 228.1096 0072039 67.5449 325.7694 13.35325940931589Epoch: 2025-11-06T18:19Z
TLE epoch observation values (Epoch: 2025-11-06T18:19:34.760Z)
Latitude
32.90492°
Longitude
-92.99263°
Altitude
1,086.463 km
Speed
7.334 km/s
True Right ascension
15h 12m 28s
True Declination
32° 45' 19"
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
04:03:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,177.856 km
Perigee altitude
1,069.769 km
Semi-major axis
7,501.949 km
Eccentricity
0.0072
Inclination
89.9847°
RAAN
228.1096°
Arg. of periapsis
67.5449°
True anomaly
325.30156°
Mean anomaly
325.7694°
Eccentric anomaly
325.53583°
Mean motion
3.34027 °/min
Orbital period
107.78 mins
BSTAR
0.00024143
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-07 17:40:41.095Z | 119.524° SE | 2025-11-07 17:44:41.095Z | 79.775° E | 21.186° | 2025-11-07 17:49:41.095Z | 27.604° NE |
| 11 mins | 2025-11-07 19:27:41.095Z | 199.572° SSW | 2025-11-07 19:32:41.095Z | 286.057° WNW | 39.323° | 2025-11-07 19:38:41.095Z | 349.075° N |
| 13 mins | 2025-11-08 06:42:41.095Z | 5.791° NNE | 2025-11-08 06:49:41.095Z | 112.153° ESE | 43.727° | 2025-11-08 06:55:41.095Z | 175.846° 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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