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NOAA 6, 11416

Orbit data source: Space-Track

NOAA 6, 11416 is a payload satellite owned by NOAA (US) in SSO that was launched on Wed, 27 Jun 1979 UTC via an ATLAS F 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
11416, 1979-057A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS N, STAR 37S
Mass
1,418 kg wet, 684 kg dry
Launch date (UTC)
1979-06-27 (47 years ago)
Launch vehicle
ATLAS F
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: 4 hours ago

TLE from 4 hours ago
0 NOAA 6
1 11416U 79057A   26007.83710854  .00000386  00000-0  14998-3 0  9993
2 11416  98.5812  38.3431 0010122  19.8541 340.3036 14.35379012427955
Epoch: 2026-01-07T20:05Z
TLE epoch observation values (Epoch: 2026-01-07T20:05:26.177Z)
Latitude
-0.00009°
Longitude
-10.41579°
Altitude
769.931 km
Speed
7.473 km/s
True Right ascension
02h 33m 22s
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
00:14:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
778.175 km
Perigee altitude
763.703 km
Semi-major axis
7,149.076 km
Eccentricity
0.00101
Inclination
98.5812°
RAAN
38.3431°
Arg. of periapsis
19.8541°
True anomaly
340.26446°
Mean anomaly
340.3036°
Eccentric anomaly
340.28404°
Mean motion
3.59061 °/min
Orbital period
100.26 mins
BSTAR
0.00014998
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