OPS 2366 (TRANSIT 14), 2401
Orbit data source: Space-Track
OPS 2366 (TRANSIT 14), 2401 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Thu, 18 Aug 1966 UTC via an SCOUT A 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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2401 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~49 kg wet, ~49 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: 12 hours ago
TLE from 12 hours ago
0 OPS 2366 (TRANSIT 14)
1 02401U 66076A 26120.86962830 .00000137 00000-0 18317-3 0 9999
2 02401 88.8459 71.3440 0034780 82.4370 331.5443 13.53946037944692Epoch: 2026-04-30T20:52Z
TLE epoch observation values (Epoch: 2026-04-30T20:52:15.885Z)
Latitude
53.86959°
Longitude
-98.95907°
Altitude
1,043.974 km
Speed
7.346 km/s
True Right ascension
04h 51m 40s
True Declination
53° 42' 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
16:49:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,080.675 km
Perigee altitude
1,028.971 km
Semi-major axis
7,432.96 km
Eccentricity
0.00348
Inclination
88.8459°
RAAN
71.344°
Arg. of periapsis
82.437°
True anomaly
331.35367°
Mean anomaly
331.5443°
Eccentric anomaly
331.44906°
Mean motion
3.38689 °/min
Orbital period
106.29 mins
BSTAR
0.00018317
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Other satellites on launch #76 in the year 1966 (1966-08-18 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 2366 (TRANSIT 14) 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 | 2026-05-01 09:36:43.488Z | 346.899° N | 2026-05-01 09:42:43.488Z | 268.391° W | 35.667° | 2026-05-01 09:47:43.488Z | 209.628° SW |
| 8 mins | 2026-05-01 19:48:43.488Z | 114.903° SE | 2026-05-01 19:52:43.488Z | 69.309° E | 20.77° | 2026-05-01 19:56:43.488Z | 29.322° NE |
| 10 mins | 2026-05-01 21:33:43.488Z | 201.855° SSW | 2026-05-01 21:37:43.488Z | 260.54° W | 39.191° | 2026-05-01 21:43:43.488Z | 348.679° N |
| 11 mins | 2026-05-02 08:40:43.488Z | 6.869° NNE | 2026-05-02 08:45:43.488Z | 70.314° E | 43.264° | 2026-05-02 08:51:43.488Z | 172.601° S |
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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