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: 5 hours ago
TLE from 5 hours ago
0 NOAA 6
1 11416U 79057A 26044.50303543 .00000349 00000-0 13682-3 0 9999
2 11416 98.5783 74.7998 0008707 263.9350 96.0843 14.35414890433211Epoch: 2026-02-13T12:04Z
TLE epoch observation values (Epoch: 2026-02-13T12:04:22.261Z)
Latitude
-0.00003°
Longitude
110.16754°
Altitude
777.293 km
Speed
7.465 km/s
True Right ascension
04h 59m 11s
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
20:02:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
777.044 km
Perigee altitude
764.595 km
Semi-major axis
7,148.957 km
Eccentricity
0.00087
Inclination
98.5783°
RAAN
74.7998°
Arg. of periapsis
263.935°
True anomaly
96.1835°
Mean anomaly
96.0843°
Eccentric anomaly
96.1339°
Mean motion
3.5907 °/min
Orbital period
100.26 mins
BSTAR
0.00013682
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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 | 2026-02-14 01:34:30.184Z | 150.93° SSE | 2026-02-14 01:38:30.184Z | 96.404° ESE | 40.738° | 2026-02-14 01:43:30.184Z | 354.72° N |
| 5 mins | 2026-02-14 13:47:30.184Z | 63.229° ENE | 2026-02-14 13:49:30.184Z | 93.963° ESE | 20.284° | 2026-02-14 13:52:30.184Z | 136.031° SSE |
| 8 mins | 2026-02-14 15:25:30.184Z | 351.47° N | 2026-02-14 15:28:30.184Z | 299.104° NW | 33.899° | 2026-02-14 15:33:30.184Z | 220.229° 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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