Showing default

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.

Loading next visibility...
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: 16 hours ago

TLE from 16 hours ago
0 TIROS 1
1    29U 60002B   25321.68434838  .00001327  00000-0  20883-3 0  9993
2    29  48.3791 309.5212 0021856  77.0891 283.2461 14.78352749510834
Epoch: 2025-11-17T16:25Z
TLE epoch observation values (Epoch: 2025-11-17T16:25:27.700Z)
Latitude
-0.00007°
Longitude
6.17446°
Altitude
631.416 km
Speed
7.546 km/s
True Right ascension
20h 38m 05s
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
05:04:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.878 km
Perigee altitude
620.22 km
Semi-major axis
7,013.686 km
Eccentricity
0.00219
Inclination
48.3791°
RAAN
309.5212°
Arg. of periapsis
77.0891°
True anomaly
283.00216°
Mean anomaly
283.2461°
Eccentric anomaly
283.12415°
Mean motion
3.69508 °/min
Orbital period
97.43 mins
BSTAR
0.00020883
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)

Documentation

Showing up to 5 results
|