Showing default

OPS 6026 (DMSP 4A F1), 2418

Orbit data source: Space-Track

OPS 6026 (DMSP 4A F1), 2418 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Fri, 16 Sep 1966 UTC via a THOR BURNER 2 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
2418, 1966-082A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
DMSP BLOCK 4A, Unknown motor
Mass
79 kg wet, 79 kg dry
Launch date (UTC)
1966-09-16 (60 years ago)
Launch vehicle
THOR BURNER 2
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 OPS 6026 (DMSP 4A F1)
1  2418U 66082A   26111.88964834  .00000271  00000-0  86195-4 0  9991
2  2418  98.3338 266.1545 0115141 194.2400 165.5537 14.43861312104160
Epoch: 2026-04-21T21:21Z
TLE epoch observation values (Epoch: 2026-04-21T21:21:05.616Z)
Latitude
-0.00002°
Longitude
95.92215°
Altitude
828.234 km
Speed
7.397 km/s
True Right ascension
17h 44m 37s
True Declination
0° 00' 00"
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
18:44:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.87 km
Perigee altitude
660.885 km
Semi-major axis
7,121.015 km
Eccentricity
0.01151
Inclination
98.3338°
RAAN
266.1545°
Arg. of periapsis
194.24°
True anomaly
165.87833°
Mean anomaly
165.5537°
Eccentric anomaly
165.71646°
Mean motion
3.61186 °/min
Orbital period
99.67 mins
BSTAR
0.000086195
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...
Other satellites on launch #82 in the year 1966 (1966-09-16 UTC)

Documentation

Showing up to 5 results
|