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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). 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
978, 1965-004A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS I, Unknown motor
Mass
138 kg wet, 138 kg dry
Launch date (UTC)
1965-01-22 (61 years ago)
Launch vehicle
THOR DELTA C
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 TIROS 9
1 00978U 65004A   25318.26752015  .00000149  00000-0  19631-3 0  9993
2 00978  96.4027 207.7245 1158605 139.7261 229.5745 12.11121524685593
Epoch: 2025-11-14T06:25Z
TLE epoch observation values (Epoch: 2025-11-14T06:25:13.740Z)
Latitude
-0.00005°
Longitude
57.80379°
Altitude
2,291.785 km
Speed
6.497 km/s
True Right ascension
13h 50m 53s
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
14:45:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,556.435 km
Perigee altitude
701.071 km
Semi-major axis
8,006.89 km
Eccentricity
0.11586
Inclination
96.4027°
RAAN
207.7245°
Arg. of periapsis
139.7261°
True anomaly
220.37704°
Mean anomaly
229.5745°
Eccentric anomaly
224.88956°
Mean motion
3.02934 °/min
Orbital period
118.84 mins
BSTAR
0.00019631
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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