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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   26193.40577765 -.00000152  00000-0 -16863-3 0  9998
2 00978  96.4057 331.0459 1157395 340.5475  15.4655 12.11147884714668
Epoch: 2026-07-12T09:44Z
TLE epoch observation values (Epoch: 2026-07-12T09:44:19.188Z)
Latitude
-0.00015°
Longitude
-105.33914°
Altitude
749.605 km
Speed
7.882 km/s
True Right ascension
22h 04m 11s
True Declination
0° 00' 01"
Sunlit
Object was in full shadow 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
10:27:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,555.337 km
Perigee altitude
701.937 km
Semi-major axis
8,006.774 km
Eccentricity
0.11574
Inclination
96.4057°
RAAN
331.0459°
Arg. of periapsis
340.5475°
True anomaly
19.56716°
Mean anomaly
15.4655°
Eccentric anomaly
17.45458°
Mean motion
3.0294 °/min
Orbital period
118.84 mins
BSTAR
-0.00016863
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Other satellites on launch #4 in the year 1965 (1965-01-22 UTC)

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