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: 17 hours ago
TLE from 17 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 26020.11294741 .00000106 00000-0 18956-3 0 9991
2 01514 89.9826 228.0084 0069068 216.8560 259.5518 13.35341979941505Epoch: 2026-01-20T02:42Z
TLE epoch observation values (Epoch: 2026-01-20T02:42:38.656Z)
Latitude
64.45137°
Longitude
-112.18837°
Altitude
1,147.622 km
Speed
7.28 km/s
True Right ascension
03h 11m 53s
True Declination
64° 19' 27"
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
20:19:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,175.566 km
Perigee altitude
1,071.938 km
Semi-major axis
7,501.889 km
Eccentricity
0.00691
Inclination
89.9826°
RAAN
228.0084°
Arg. of periapsis
216.856°
True anomaly
258.7747°
Mean anomaly
259.5518°
Eccentric anomaly
259.16313°
Mean motion
3.34031 °/min
Orbital period
107.77 mins
BSTAR
0.00018956
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-01-21 00:20:42.297Z | 44.596° NE | 2026-01-21 00:23:42.297Z | 70.996° E | 13.747° | 2026-01-21 00:26:42.297Z | 99.021° ESE |
| 11 mins | 2026-01-21 02:07:42.297Z | 1.37° NNE | 2026-01-21 02:12:42.297Z | 257.701° W | 44.966° | 2026-01-21 02:18:42.297Z | 185.504° SSW |
| 4 mins | 2026-01-21 03:57:42.297Z | 305.862° NW | 2026-01-21 03:58:42.297Z | 296.612° NW | 13.161° | 2026-01-21 04:01:42.297Z | 269.119° W |
| 7 mins | 2026-01-21 12:27:42.297Z | 101.296° ESE | 2026-01-21 12:30:42.297Z | 73.405° E | 17.179° | 2026-01-21 12:34:42.297Z | 36.378° NE |
| 13 mins | 2026-01-21 14:11:42.297Z | 182.073° SSW | 2026-01-21 14:17:42.297Z | 264.278° W | 44.465° | 2026-01-21 14:24:42.297Z | 355.331° N |
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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