TECHEDSAT-11, 60208 (Decayed)
Orbit data source: Space-Track
TECHEDSAT-11, 60208 was an American payload satellite in LEO that was launched on Thu, 04 Jul 2024 UTC via an FIREFLY ALPHA 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.
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60208 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ARC
Mission
Decayed Civil Technology
Bus & Motor
CUBESAT 6UXL, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Sail, 1.0 m
Radar Cross Section
0.045 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 TECHEDSAT-11
1 60208U 24125F 26046.49759830 .22159603 22509-5 50511-2 0 9998
2 60208 97.2328 260.3655 0009466 338.6387 21.4511 16.29991395 90512Epoch: 2026-02-15T11:56Z
TLE epoch observation values (Epoch: 2026-02-15T11:56:32.493Z)
Latitude
-0.00001°
Longitude
-64.27533°
Altitude
190.016 km
Speed
7.796 km/s
True Right ascension
17h 21m 27s
True Declination
0° 00' 00"
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
06:42:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
195.593 km
Perigee altitude
183.159 km
Semi-major axis
6,567.513 km
Eccentricity
0.00095
Inclination
97.2328°
RAAN
260.3655°
Arg. of periapsis
338.6387°
True anomaly
21.49081°
Mean anomaly
21.4511°
Eccentric anomaly
21.47095°
Mean motion
4.07795 °/min
Orbital period
88.28 mins
BSTAR
0.0050511
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Other satellites on launch #125 in the year 2024 (2024-07-04 UTC)
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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.TECHEDSAT-11 Visibility
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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. |
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| This satellite is decayed. |
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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