Showing default

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.

Loading next visibility...
Identifier
2401, 1966-076A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~49 kg wet, ~49 kg dry
Launch date (UTC)
1966-08-18 (59 years ago)
Launch vehicle
SCOUT A
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 OPS 2366 (TRANSIT 14)
1 02401U 66076A   26035.13345650  .00000152  00000-0  20653-3 0  9992
2 02401  88.8418  81.4262 0031360 334.4824  36.1492 13.53924178933092
Epoch: 2026-02-04T03:12Z
TLE epoch observation values (Epoch: 2026-02-04T03:12:10.641Z)
Latitude
10.79137°
Longitude
-100.7029°
Altitude
1,041.253 km
Speed
7.341 km/s
True Right ascension
05h 26m 35s
True Declination
10° 43' 51"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:30:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.213 km
Perigee altitude
1,031.593 km
Semi-major axis
7,433.04 km
Eccentricity
0.00314
Inclination
88.8418°
RAAN
81.4262°
Arg. of periapsis
334.4824°
True anomaly
36.36185°
Mean anomaly
36.1492°
Eccentric anomaly
36.25546°
Mean motion
3.38683 °/min
Orbital period
106.29 mins
BSTAR
0.00020653
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|