TECHEDSAT-11, 60208
Orbit data source: Space-Track
TECHEDSAT-11, 60208 is an American payload satellite in SSO 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ARC
Mission
Operational 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: 15 hours ago
TLE from 15 hours ago
0 TECHEDSAT-11
1 60208U 24125F 25293.84051012 .00023179 00000-0 64461-3 0 9998
2 60208 97.2626 142.8876 0019886 20.6275 339.5767 15.36646114 72354Epoch: 2025-10-20T20:10Z
TLE epoch observation values (Epoch: 2025-10-20T20:10:20.074Z)
Latitude
-0.00011°
Longitude
170.76692°
Altitude
446.417 km
Speed
7.651 km/s
True Right ascension
09h 31m 33s
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
06:07:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.557 km
Perigee altitude
439.389 km
Semi-major axis
6,831.11 km
Eccentricity
0.00199
Inclination
97.2626°
RAAN
142.8876°
Arg. of periapsis
20.6275°
True anomaly
339.497°
Mean anomaly
339.5767°
Eccentric anomaly
339.53687°
Mean motion
3.8442 °/min
Orbital period
93.65 mins
BSTAR
0.00064461
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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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-21 13:30:10.138Z | 127.048° SE | 2025-10-21 13:33:10.138Z | 57.329° ENE | 22.85° | 2025-10-21 13:35:10.138Z | 17.555° NNE |
| 4 mins | 2025-10-22 02:27:10.138Z | 55.094° ENE | 2025-10-22 02:28:10.138Z | 84.739° E | 27.745° | 2025-10-22 02:31:10.138Z | 159.354° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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