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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 (67 years ago)
Launch vehicle
THOR ABLE II
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 TIROS 1
1    29U 60002B   26317.85770286  .00000586  00000-0  10715-3 0  9997
2    29  48.3793  33.2530 0022345 195.2700 164.7542 14.78937134564284
Epoch: 2026-11-13T20:35Z
TLE epoch observation values (Epoch: 2026-11-13T20:35:05.527Z)
Latitude
0.00003°
Longitude
31.50917°
Altitude
648.164 km
Speed
7.527 km/s
True Right ascension
02h 13m 00s
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
22:57:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
649.369 km
Perigee altitude
618.034 km
Semi-major axis
7,011.839 km
Eccentricity
0.00223
Inclination
48.3793°
RAAN
33.253°
Arg. of periapsis
195.27°
True anomaly
164.82135°
Mean anomaly
164.7542°
Eccentric anomaly
164.78779°
Mean motion
3.69654 °/min
Orbital period
97.39 mins
BSTAR
0.00010715
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Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

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