TIROS 9, 978
Orbit data source: Space-Track
TIROS 9, 978 is a payload satellite owned by GSFC (US) in SSO that was launched on Fri, 22 Jan 1965 UTC via a THOR DELTA C launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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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Edit Public Description
Identifier | |
Orbit | SSO |
Last TLE update | 1 day ago |
Origin | |
Manufacturer | RCA/East Windsor |
Mission | Non-operational Civil Weather |
Bus & Motor | TIROS I, Unknown motor |
Mass | 138 kg wet, 138 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 1.07 m |
Radar Cross Section | 0.920 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 TIROS 9
1 00978U 65004A 25083.98108002 .00000208 00000-0 29196-3 0 9995
2 00978 96.3940 87.3354 1156751 286.3043 61.4042 12.11095890657235
Epoch: 2025-03-24T23:32Z
Definitive object data (Epoch: 2025-03-24T23:32:45.313Z)
Latitude | -0.00002° |
Longitude | -88.54305° |
Altitude | 1,280.11 km |
Speed | 7.374 km/s |
True Right ascension | 05h 49m 20s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 70.14304° |
Longitude | -105.97901° |
Altitude | 2,387.202 km |
Speed | 6.429 km/s |
Apparent Right ascension | 21h 18m 05s |
Apparent Declination | 54° 18' 01" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 06:58:48 |
Azimuth | 340.294° N |
Elevation | 8.839° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 2,555.077 km |
Perigee altitude | 702.655 km |
Semi-major axis | 8,007.003 km |
Eccentricity | 0.1156751 |
Inclination | 96.394° |
RAAN | 87.3354° |
Arg. of periapsis | 286.3043° |
True anomaly | 73.80685° |
Mean anomaly | 61.4042° |
Eccentric anomaly | 67.52866° |
Mean motion | 3.02927 °/min |
BSTAR | 0.00029196 |
Orbital period | 118.84 mins |
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)
DELTA 1 R/B, 979 |
DELTA 1 DEB, 1312 |
DELTA 1 DEB, 1313 |
DELTA 1 DEB, 27720 |
TIROS 9 Visibility forecast
Observer location: undefined°, undefined°
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. |
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8 mins | 2025-03-26 10:02:13.537Z | 49.078° ENE | 2025-03-26 10:06:13.537Z | 66.94° ENE | 11.995° | 2025-03-26 10:10:13.537Z | 86.154° E |
23 mins | 2025-03-26 11:55:13.537Z | 18.085° NNE | 2025-03-26 12:07:13.537Z | 87.978° E | 39.83° | 2025-03-26 12:18:13.537Z | 168.758° S |
21 mins | 2025-03-26 13:53:13.537Z | 359.648° N | 2025-03-26 14:04:13.537Z | 296.677° NW | 36.996° | 2025-03-26 14:14:13.537Z | 228.723° WSW |
10 mins | 2025-03-26 15:53:13.537Z | 338.85° N | 2025-03-26 15:57:13.537Z | 320.906° NNW | 14.221° | 2025-03-26 16:03:13.537Z | 292.976° NW |
10 mins | 2025-03-26 21:24:13.537Z | 65.653° ENE | 2025-03-26 21:28:13.537Z | 44.101° NE | 14.613° | 2025-03-26 21:34:13.537Z | 15.422° NNE |
20 mins | 2025-03-26 23:14:13.537Z | 136.742° SSE | 2025-03-26 23:22:13.537Z | 67.96° E | 38.781° | 2025-03-26 23:34:13.537Z | 356.619° N |
19 mins | 2025-03-27 01:12:13.537Z | 206.746° SW | 2025-03-27 01:20:13.537Z | 277.115° WNW | 34.762° | 2025-03-27 01:31:13.537Z | 339.993° N |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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