Showing default

OPS 4078 (DMSP 4B F2), 3510

Orbit data source: Space-Track

OPS 4078 (DMSP 4B F2), 3510 is a payload satellite owned by SAMSO (US) in SSO that was launched on Wed, 23 Oct 1968 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
3510, 1968-092A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
DMSP BLOCK 4B, Unknown motor
Mass
79 kg wet, 79 kg dry
Launch date (UTC)
1968-10-23 (57 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: 10 hours ago

TLE from 10 hours ago
0 OPS 4078 (DMSP 4B F2)
1 03510U 68092A   26002.33137178  .00000337  00000-0  15174-3 0  9991
2 03510  98.5519 128.0905 0030838  94.1386 266.3321 14.28188274973575
Epoch: 2026-01-02T07:57Z
TLE epoch observation values (Epoch: 2026-01-02T07:57:10.521Z)
Latitude
-0.00004°
Longitude
-93.17645°
Altitude
802.208 km
Speed
7.452 km/s
True Right ascension
08h 32m 21s
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
17:50:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
817.054 km
Perigee altitude
772.813 km
Semi-major axis
7,173.07 km
Eccentricity
0.00308
Inclination
98.5519°
RAAN
128.0905°
Arg. of periapsis
94.1386°
True anomaly
265.97954°
Mean anomaly
266.3321°
Eccentric anomaly
266.15581°
Mean motion
3.57261 °/min
Orbital period
100.77 mins
BSTAR
0.00015174
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 #92 in the year 1968 (1968-10-23 UTC)

Documentation

Showing up to 5 results
|