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: 1 day ago
TLE from 1 day ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 26009.68747285 .00000066 00000-0 11186-3 0 9999
2 01514 89.9831 228.0241 0068614 246.8621 181.2960 13.35340342940114Epoch: 2026-01-09T16:29Z
TLE epoch observation values (Epoch: 2026-01-09T16:29:57.654Z)
Latitude
68.21389°
Longitude
-128.6477°
Altitude
1,190.067 km
Speed
7.24 km/s
True Right ascension
15h 12m 15s
True Declination
68° 06' 07"
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
22:24:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,175.232 km
Perigee altitude
1,072.285 km
Semi-major axis
7,501.895 km
Eccentricity
0.00686
Inclination
89.9831°
RAAN
228.0241°
Arg. of periapsis
246.8621°
True anomaly
181.27837°
Mean anomaly
181.296°
Eccentric anomaly
181.28717°
Mean motion
3.34031 °/min
Orbital period
107.77 mins
BSTAR
0.00011186
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-01-11 01:09:13.868Z | 38.234° NE | 2026-01-11 01:13:13.868Z | 74.456° E | 16.948° | 2026-01-11 01:17:13.868Z | 112.531° SE |
| 12 mins | 2026-01-11 02:56:13.868Z | 357.432° N | 2026-01-11 03:02:13.868Z | 243.916° WSW | 43.685° | 2026-01-11 03:08:13.868Z | 191.834° SSW |
| 8 mins | 2026-01-11 13:16:13.868Z | 108.309° ESE | 2026-01-11 13:20:13.868Z | 68.085° E | 19.928° | 2026-01-11 13:24:13.868Z | 30.948° NE |
| 12 mins | 2026-01-11 15:01:13.868Z | 189.614° SSW | 2026-01-11 15:07:13.868Z | 291.32° WNW | 42.47° | 2026-01-11 15:13:13.868Z | 351.642° 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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