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NOAA 3, 6920

Orbit data source: Space-Track

NOAA 3, 6920 is a payload satellite owned by NOAA (US) in SSO that was launched on Tue, 06 Nov 1973 UTC via a DELTA 0300 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.

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Identifier
6920, 1973-086A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS M, Unknown motor
Mass
340 kg wet, 340 kg dry
Launch date (UTC)
1973-11-06 (52 years ago)
Launch vehicle
DELTA 0300
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

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

TLE from 8 hours ago
0 NOAA 3
1  6920U 73086A   26033.52776576 -.00000035  00000-0  81348-4 0  9997
2  6920 102.2909  46.1653 0006416  14.4886 140.1274 12.40390767365209
Epoch: 2026-02-02T12:39Z
TLE epoch observation values (Epoch: 2026-02-02T12:39:58.961Z)
Latitude
24.74433°
Longitude
-90.81743°
Altitude
1,511.492 km
Speed
7.11 km/s
True Right ascension
15h 27m 36s
True Declination
24° 37' 35"
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
22:56:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,507.595 km
Perigee altitude
1,497.483 km
Semi-major axis
7,880.676 km
Eccentricity
0.00064
Inclination
102.2909°
RAAN
46.1653°
Arg. of periapsis
14.4886°
True anomaly
140.1745°
Mean anomaly
140.1274°
Eccentric anomaly
140.15096°
Mean motion
3.1024 °/min
Orbital period
116.04 mins
BSTAR
0.000081348
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