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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11416 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 NOAA 6
1 11416U 79057A 26134.07356492 .00000167 00000-0 73440-4 0 9999
2 11416 98.5654 163.8012 0009857 6.7491 353.3826 14.35476322446066Epoch: 2026-05-14T01:45Z
TLE epoch observation values (Epoch: 2026-05-14T01:45:56.009Z)
Latitude
0.00005°
Longitude
-94.50665°
Altitude
769.42 km
Speed
7.473 km/s
True Right ascension
10h 55m 12s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:57:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
777.661 km
Perigee altitude
763.568 km
Semi-major axis
7,148.752 km
Eccentricity
0.00099
Inclination
98.5654°
RAAN
163.8012°
Arg. of periapsis
6.7491°
True anomaly
353.36957°
Mean anomaly
353.3826°
Eccentric anomaly
353.37609°
Mean motion
3.59085 °/min
Orbital period
100.25 mins
BSTAR
0.00007344
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Other satellites on launch #57 in the year 1979 (1979-06-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NOAA 6 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-15 01:18:38.161Z | 136.522° SSE | 2026-05-15 01:22:38.161Z | 79.493° E | 32.656° | 2026-05-15 01:27:38.161Z | 1.845° NNE |
| 6 mins | 2026-05-15 02:59:38.161Z | 227.027° WSW | 2026-05-15 03:02:38.161Z | 273.144° WNW | 20.758° | 2026-05-15 03:05:38.161Z | 312.807° NW |
| 4 mins | 2026-05-15 13:31:38.161Z | 71.112° E | 2026-05-15 13:33:38.161Z | 96.554° ESE | 13.644° | 2026-05-15 13:35:38.161Z | 120.275° SE |
| 8 mins | 2026-05-15 15:09:38.161Z | 1.957° NNE | 2026-05-15 15:12:38.161Z | 295.593° NW | 42.084° | 2026-05-15 15:17:38.161Z | 206.327° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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