Showing default

LANDSAT 1 (ERTS 1), 6126

Orbit data source: Space-Track

LANDSAT 1 (ERTS 1), 6126 is a payload satellite owned by GSFC (US) in SSO that was launched on Sun, 23 Jul 1972 UTC via a DELTA 0900 launch vehicle from the Air Force Western Test Range (AFWTR). 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
6126, 1972-058A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
GE/MSVD
Mission
Non-operational spacecraft
Bus & Motor
NIMBUS, Unknown motor
Mass
891 kg wet, 891 kg dry
Launch date (UTC)
1972-07-23 (54 years ago)
Launch vehicle
DELTA 0900
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

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

TLE from 6 days ago
0 LANDSAT 1 (ERTS 1)
1 06126U 72058A   26155.07687136  .00000286  00000-0  23513-3 0  9997
2 06126  99.3366 184.5989 0006912 294.8179  65.2264 13.97834600746121
Epoch: 2026-06-04T01:50Z
TLE epoch observation values (Epoch: 2026-06-04T01:50:41.685Z)
Latitude
-0.00002°
Longitude
-95.60111°
Altitude
902.061 km
Speed
7.402 km/s
True Right ascension
12h 18m 23s
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
07:39:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
903.552 km
Perigee altitude
893.493 km
Semi-major axis
7,276.659 km
Eccentricity
0.00069
Inclination
99.3366°
RAAN
184.5989°
Arg. of periapsis
294.8179°
True anomaly
65.29834°
Mean anomaly
65.2264°
Eccentric anomaly
65.26237°
Mean motion
3.49659 °/min
Orbital period
102.96 mins
BSTAR
0.00023513
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|