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.
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68126 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ECHOSTAR 25
1 68126U 26045A 26102.21951169 .00000060 00000-0 00000-0 0 9991
2 68126 0.0191 289.8577 0002127 154.2786 66.4643 1.00272988 339Epoch: 2026-04-12T05:16Z
TLE epoch observation values (Epoch: 2026-04-12T05:16:05.810Z)
Latitude
-0.02192°
Longitude
-128.82861°
Altitude
35,782.207 km
Speed
3.075 km/s
True Right ascension
10h 02m 29s
True Declination
0° 01' 19"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:35:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,796.297 km
Perigee altitude
35,778.36 km
Semi-major axis
42,165.465 km
Eccentricity
0.00021
Inclination
0.0191°
RAAN
289.8577°
Arg. of periapsis
154.2786°
True anomaly
66.48665°
Mean anomaly
66.4643°
Eccentric anomaly
66.47547°
Mean motion
0.25067 °/min
Orbital period
1,436.13 mins
BSTAR
0
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Other satellites on launch #45 in the year 2026 (2026-03-10 UTC)
No other RSOs were in this launch
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ECHOSTAR 25 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-04-12 13:12:53.321Z | 214.436° SW | 2026-04-13 13:12:53.321Z | 214.432° SW | 31.476° | 2026-04-13 13:12:53.321Z | 214.432° SW |
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68126 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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