OPS 8480 (TRANSIT 5B-6), 1420
Orbit data source: Space-Track
OPS 8480 (TRANSIT 5B-6), 1420 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Thu, 24 Jun 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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1420 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
APL
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
OCT CYL + 4 PAN + ANT, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OPS 8480 (TRANSIT 5B-6)
1 1420U 65048A 26305.45303148 .00000133 00000-0 18500-3 0 9998
2 1420 89.8704 284.4462 0074642 34.3782 119.9397 13.51929091 22008Epoch: 2026-11-01T10:52Z
TLE epoch observation values (Epoch: 2026-11-01T10:52:21.919Z)
Latitude
24.96978°
Longitude
-99.44936°
Altitude
1,096.293 km
Speed
7.292 km/s
True Right ascension
06h 57m 32s
True Declination
24° 50' 40"
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
17:54:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,117.753 km
Perigee altitude
1,006.68 km
Semi-major axis
7,440.353 km
Eccentricity
0.00746
Inclination
89.8704°
RAAN
284.4462°
Arg. of periapsis
34.3782°
True anomaly
120.67743°
Mean anomaly
119.9397°
Eccentric anomaly
120.30891°
Mean motion
3.38184 °/min
Orbital period
106.45 mins
BSTAR
0.000185
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Other satellites on launch #48 in the year 1965 (1965-06-24 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 8480 (TRANSIT 5B-6) 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 | 2026-11-01 22:38:41.834Z | 156.855° SSE | 2026-11-01 22:44:41.834Z | 80.314° E | 53.7° | 2026-11-01 22:50:41.834Z | 7.735° NNE |
| 8 mins | 2026-11-02 00:27:41.834Z | 238.712° WSW | 2026-11-02 00:31:41.834Z | 284.708° WNW | 21.995° | 2026-11-02 00:35:41.834Z | 326.369° NNW |
| 8 mins | 2026-11-02 09:49:41.834Z | 40.989° NE | 2026-11-02 09:53:41.834Z | 87° E | 23.512° | 2026-11-02 09:57:41.834Z | 127.333° SE |
| 11 mins | 2026-11-02 11:34:41.834Z | 349.677° N | 2026-11-02 11:39:41.834Z | 283.664° WNW | 55.153° | 2026-11-02 11:45:41.834Z | 203.875° SW |
| 7 mins | 2026-11-02 21:47:41.834Z | 108.968° ESE | 2026-11-02 21:50:41.834Z | 74.319° E | 21.585° | 2026-11-02 21:54:41.834Z | 31.359° NE |
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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