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: 9 hours ago
TLE from 9 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 25331.96473332 .00000111 00000-0 19878-3 0 9993
2 01514 89.9856 228.0816 0070831 8.9057 2.4396 13.35331683934414Epoch: 2025-11-27T23:09Z
TLE epoch observation values (Epoch: 2025-11-27T23:09:12.958Z)
Latitude
11.33309°
Longitude
173.66639°
Altitude
1,075.779 km
Speed
7.341 km/s
True Right ascension
15h 12m 20s
True Declination
11° 16' 11"
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
05:28:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,176.928 km
Perigee altitude
1,070.654 km
Semi-major axis
7,501.928 km
Eccentricity
0.00708
Inclination
89.9856°
RAAN
228.0816°
Arg. of periapsis
8.9057°
True anomaly
2.47446°
Mean anomaly
2.4396°
Eccentric anomaly
2.457°
Mean motion
3.34029 °/min
Orbital period
107.78 mins
BSTAR
0.00019878
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-28 17:10:59.127Z | 159.067° S | 2025-11-28 17:16:59.127Z | 74.868° E | 40.777° | 2025-11-28 17:22:59.127Z | 6.067° NNE |
| 7 mins | 2025-11-28 19:01:59.127Z | 248.294° W | 2025-11-28 19:04:59.127Z | 281.917° WNW | 19.921° | 2025-11-28 19:08:59.127Z | 322.829° NNW |
| 11 mins | 2025-11-29 04:28:59.127Z | 28.574° NE | 2025-11-29 04:33:59.127Z | 83.688° E | 27.299° | 2025-11-29 04:39:59.127Z | 142.606° SSE |
| 11 mins | 2025-11-29 06:16:59.127Z | 342.452° N | 2025-11-29 06:21:59.127Z | 272.765° WNW | 35.385° | 2025-11-29 06:27:59.127Z | 211.305° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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