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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 spacecraft
Bus & Motor
TIROS, Unknown motor
Mass
122 kg wet, 122 kg dry
Launch date (UTC)
1960-04-01 (66 years ago)
Launch vehicle
THOR ABLE II
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: 11 hours ago

TLE from 11 hours ago
0 TIROS 1
1    29U 60002B   25306.47669671  .00000871  00000-0  14725-3 0  9999
2    29  48.3795  21.7430 0022249  10.5987 349.5391 14.78302712508580
Epoch: 2025-11-02T11:26Z
TLE epoch observation values (Epoch: 2025-11-02T11:26:26.595Z)
Latitude
-0.00005°
Longitude
168.14027°
Altitude
619.713 km
Speed
7.559 km/s
True Right ascension
01h 26m 58s
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
18:23:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.312 km
Perigee altitude
620.102 km
Semi-major axis
7,013.844 km
Eccentricity
0.00222
Inclination
48.3795°
RAAN
21.743°
Arg. of periapsis
10.5987°
True anomaly
349.49268°
Mean anomaly
349.5391°
Eccentric anomaly
349.5159°
Mean motion
3.69495 °/min
Orbital period
97.43 mins
BSTAR
0.00014725
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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