THOR ALTAIR R/B, 1583

Orbit data source: Space-Track

THOR ALTAIR R/B, 1583 is space debris in SSO originally from a launch on Fri, 10 Sep 1965 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
1583, 1965-072D
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
1965-09-10 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 THOR ALTAIR R/B
1 01583U 65072D   25243.20642362  .00002981  00000-0  50117-3 0  9995
2 01583  98.4286 106.5891 0144091  59.3566 302.1751 14.63754306124509
Epoch: 2025-08-31T04:57Z
TLE epoch observation values (Epoch: 2025-08-31T04:57:15Z)
Latitude
-0.00002°
Longitude
52.64691°
Altitude
630.947 km
Speed
7.571 km/s
True Right ascension
07h 06m 21s
True Declination
0° 00' 00"
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
05:03:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
779.838 km
Perigee altitude
576.489 km
Semi-major axis
7,056.301 km
Eccentricity
0.01441
Inclination
98.4286°
RAAN
106.5891°
Arg. of periapsis
59.3566°
True anomaly
300.76413°
Mean anomaly
302.1751°
Eccentric anomaly
301.47096°
Mean motion
3.66166 °/min
Orbital period
98.32 mins
BSTAR
0.00050117
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