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 25355.21610619 .00000078 00000-0 13566-3 0 9998
2 01514 89.9844 228.0513 0068960 303.0330 176.8770 13.35336737937519Epoch: 2025-12-21T05:11Z
TLE epoch observation values (Epoch: 2025-12-21T05:11:11.574Z)
Latitude
60.13557°
Longitude
-119.8057°
Altitude
1,188.698 km
Speed
7.24 km/s
True Right ascension
03h 12m 05s
True Declination
59° 59' 43"
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
17:45:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,175.505 km
Perigee altitude
1,072.039 km
Semi-major axis
7,501.909 km
Eccentricity
0.0069
Inclination
89.9844°
RAAN
228.0513°
Arg. of periapsis
303.033°
True anomaly
176.91968°
Mean anomaly
176.877°
Eccentric anomaly
176.89838°
Mean motion
3.3403 °/min
Orbital period
107.77 mins
BSTAR
0.00013566
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-22 02:46:17.067Z | 27.254° NE | 2025-12-22 02:52:17.067Z | 85.765° E | 23.502° | 2025-12-22 02:57:17.067Z | 132.92° SE |
| 12 mins | 2025-12-22 04:34:17.067Z | 349.953° N | 2025-12-22 04:40:17.067Z | 264.877° W | 39.117° | 2025-12-22 04:46:17.067Z | 204.168° SW |
| 10 mins | 2025-12-22 14:53:17.067Z | 124.21° SE | 2025-12-22 14:57:17.067Z | 81.832° E | 25.433° | 2025-12-22 15:03:17.067Z | 20.51° NNE |
| 11 mins | 2025-12-22 16:40:17.067Z | 206.641° SW | 2025-12-22 16:45:17.067Z | 280.233° WNW | 36.633° | 2025-12-22 16:51:17.067Z | 345.39° N |
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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