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: 3 hours ago
TLE from 3 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 1514U 65065F 26120.20907718 .00000102 00000-0 18357-3 0 9998
2 1514 89.9963 227.9051 0068048 296.2602 126.8322 13.35361259954860Epoch: 2026-04-30T05:01Z
TLE epoch observation values (Epoch: 2026-04-30T05:01:04.268Z)
Latitude
63.79631°
Longitude
-65.51418°
Altitude
1,168.515 km
Speed
7.26 km/s
True Right ascension
15h 11m 39s
True Declination
63° 40' 02"
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
15:39:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,174.728 km
Perigee altitude
1,072.632 km
Semi-major axis
7,501.817 km
Eccentricity
0.0068
Inclination
89.9963°
RAAN
227.9051°
Arg. of periapsis
296.2602°
True anomaly
127.45315°
Mean anomaly
126.8322°
Eccentric anomaly
127.14299°
Mean motion
3.34036 °/min
Orbital period
107.77 mins
BSTAR
0.00018357
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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 | 2026-04-30 08:24:07.463Z | 210.745° SW | 2026-04-30 08:30:07.463Z | 282.469° WNW | 32.073° | 2026-04-30 08:36:07.463Z | 342.333° N |
| 7 mins | 2026-04-30 17:56:07.463Z | 48.889° ENE | 2026-04-30 17:59:07.463Z | 77.785° E | 17.071° | 2026-04-30 18:03:07.463Z | 114.105° SE |
| 12 mins | 2026-04-30 19:42:07.463Z | 357.72° N | 2026-04-30 19:47:07.463Z | 299.35° NW | 44.152° | 2026-04-30 19:54:07.463Z | 190.756° SSW |
| 8 mins | 2026-05-01 06:02:07.463Z | 105.43° ESE | 2026-05-01 06:05:07.463Z | 75.586° E | 18.976° | 2026-05-01 06:10:07.463Z | 28.871° NE |
| 12 mins | 2026-05-01 07:47:07.463Z | 189.193° SSW | 2026-05-01 07:52:07.463Z | 256.371° W | 42.91° | 2026-05-01 07:59:07.463Z | 352.71° 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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