THORAD DELTA 1 R/B, 7532

Orbit data source: Space-Track

THORAD DELTA 1 R/B, 7532 is space debris in SSO originally from a launch on Fri, 15 Nov 1974 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
7532, 1974-089D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
MDAC-HB
Mission
Spacecraft
Bus & Motor
DELTA/TR-201, Unknown motor
Mass
845 kg wet, 845 kg dry
Launch date (UTC)
1974-11-15 (52 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL + SKIRT + NOZZLE, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 THORAD DELTA 1 R/B
1 07532U 74089D   26297.16365462 -.00000035  00000-0  60320-4 0  9998
2 07532 101.7164 254.7500 0066531 311.2986  59.1956 12.39931469351015
Epoch: 2026-10-24T03:55Z
TLE epoch observation values (Epoch: 2026-10-24T03:55:39.759Z)
Latitude
10.87335°
Longitude
160.98867°
Altitude
1,482.097 km
Speed
7.135 km/s
True Right ascension
16h 49m 54s
True Declination
10° 48' 56"
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
18:08:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,556.895 km
Perigee altitude
1,452.008 km
Semi-major axis
7,882.589 km
Eccentricity
0.00665
Inclination
101.7164°
RAAN
254.75°
Arg. of periapsis
311.2986°
True anomaly
59.85322°
Mean anomaly
59.1956°
Eccentric anomaly
59.52413°
Mean motion
3.10127 °/min
Orbital period
116.08 mins
BSTAR
0.00006032
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