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
Last TLE update
9 hours ago
Origin
Manufacturer
RCA/East Windsor
Mission
Non-operational Defense Weather
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
Cone, 0.4 m
Radar Cross Section
0.985 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 OPS 4078 (DMSP 4B F2)
1 03510U 68092A   25199.60477618  .00000094  00000-0  55052-4 0  9993
2 03510  98.5340 323.9461 0029002 224.3584 135.5274 14.28096795949638
Epoch: 2025-07-18T14:30Z
TLE epoch observation values (Epoch: 2025-07-18T14:30:52.661Z)
Latitude
-0.00003°
Longitude
169.57284°
Altitude
815.915 km
Speed
7.438 km/s
True Right ascension
21h 35m 47s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
26.24501°
Longitude
165.69987°
Altitude
821.225 km
Speed
7.434 km/s
Apparent Right ascension
22h 24m 36s
Apparent Declination
-4° 48' 00"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
11:50:18
Azimuth
34.43° NE
Elevation
-49.922°
Doppler factor
1
Orbital elements
Apogee altitude
816.043 km
Perigee altitude
774.435 km
Semi-major axis
7,173.376 km
Eccentricity
0.0029
Inclination
98.534°
RAAN
323.9461°
Arg. of periapsis
224.3584°
True anomaly
135.75962°
Mean anomaly
135.5274°
Eccentric anomaly
135.64357°
Mean motion
3.57238 °/min
Orbital period
100.77 mins
BSTAR
0.000055052
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
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)
|