Showing default

ECHOSTAR 25, 68126

Orbit data source: Space-Track

ECHOSTAR 25, 68126 is a payload satellite owned by Echostar (US) in GEO that was launched on Tue, 10 Mar 2026 UTC via an FALCON 9 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
68126, 2026-045A
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
LANT
Mission
Operational spacecraft
Bus & Motor
L-1300TM, R-4D-15-300
Mass
~6,800 kg wet, 2,929 kg dry
Launch date (UTC)
2026-03-10 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 22.5 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 ECHOSTAR 25
1 68126U 26045A   26120.43725440  .00000060  00000-0  00000-0 0  9996
2 68126   0.0389  56.2657 0002540  12.0509 178.6473  1.00271810   516
Epoch: 2026-04-30T10:29Z
TLE epoch observation values (Epoch: 2026-04-30T10:29:38.780Z)
Latitude
-0.00569°
Longitude
-128.83253°
Altitude
35,796.813 km
Speed
3.074 km/s
True Right ascension
16h 27m 51s
True Declination
0° 00' 20"
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
05:38:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,798.368 km
Perigee altitude
35,776.948 km
Semi-major axis
42,165.795 km
Eccentricity
0.00025
Inclination
0.0389°
RAAN
56.2657°
Arg. of periapsis
12.0509°
True anomaly
178.64799°
Mean anomaly
178.6473°
Eccentric anomaly
178.64764°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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 #45 in the year 2026 (2026-03-10 UTC)

Documentation

Showing up to 5 results
|