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TIROS 1, 29

Orbit data source: Space-Track

TIROS 1, 29 is a payload satellite owned by GSFC (US) in LEO that was launched on Fri, 01 Apr 1960 UTC via a THOR ABLE II 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
29, 1960-002B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational Civil Weather
Bus & Motor
TIROS, Unknown motor
Mass
122 kg wet, 122 kg dry
Launch date (UTC)
1960-04-01 (65 years ago)
Launch vehicle
THOR ABLE II
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.5 m
Radar Cross Section
0.853 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 TIROS 1
1 00029U 60002B   25243.47870414  .00001065  00000-0  17428-3 0  9997
2 00029  48.3795 320.8763 0021739 101.4110 258.9247 14.78134984499264
Epoch: 2025-08-31T11:29Z
TLE epoch observation values (Epoch: 2025-08-31T11:29:20.037Z)
Latitude
-0.00001°
Longitude
168.64474°
Altitude
638.545 km
Speed
7.539 km/s
True Right ascension
21h 23m 30s
True Declination
0° 00' 00"
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
11:58:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.486 km
Perigee altitude
620.989 km
Semi-major axis
7,014.374 km
Eccentricity
0.00217
Inclination
48.3795°
RAAN
320.8763°
Arg. of periapsis
101.411°
True anomaly
258.68036°
Mean anomaly
258.9247°
Eccentric anomaly
258.80252°
Mean motion
3.69453 °/min
Orbital period
97.44 mins
BSTAR
0.00017428
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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