Showing default

INTASAT, 7531

Orbit data source: Space-Track

INTASAT, 7531 is a payload satellite owned by INTA (ES) in SSO that was launched on Fri, 15 Nov 1974 UTC via a DELTA 2310 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
7531, 1974-089C
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
INTA
Mission
Spacecraft
Bus & Motor
INTASAT, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
1974-11-15 (51 years ago)
Launch vehicle
DELTA 2310
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: 11 hours ago

TLE from 11 hours ago
0 INTASAT
1  7531U 74089C   26130.01075522 -.00000035  00000-0  73963-4 0  9999
2  7531 101.9952 141.9838 0011118 213.1652 204.8070 12.53529333355494
Epoch: 2026-05-10T00:15Z
TLE epoch observation values (Epoch: 2026-05-10T00:15:29.251Z)
Latitude
56.06956°
Longitude
-108.02506°
Altitude
1,466.804 km
Speed
7.131 km/s
True Right ascension
08h 14m 40s
True Declination
55° 55' 28"
Sunlit
Object was in daylight 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
19:34:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,456.024 km
Perigee altitude
1,438.624 km
Semi-major axis
7,825.461 km
Eccentricity
0.00111
Inclination
101.9952°
RAAN
141.9838°
Arg. of periapsis
213.1652°
True anomaly
204.75361°
Mean anomaly
204.807°
Eccentric anomaly
204.7803°
Mean motion
3.13529 °/min
Orbital period
114.82 mins
BSTAR
0.000073963
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|