SKYKRAFT-1, 55041
Orbit data source: Space-Track
SKYKRAFT-1, 55041 is a payload satellite owned by SkyKraft (AU) in SSO that was launched on Tue, 03 Jan 2023 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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55041 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
SkyKraft
Mission
Operational Commercial Technology
Bus & Motor
SKYKRAFT CARRIER, AOCS
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.065 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SKYKRAFT-1
1 55041U 23001AJ 25315.25256353 .00044376 00000-0 86304-3 0 9996
2 55041 97.3519 21.4156 0007353 138.1918 221.9895 15.47441276159146Epoch: 2025-11-11T06:03Z
TLE epoch observation values (Epoch: 2025-11-11T06:03:41.488Z)
Latitude
0°
Longitude
-120.14905°
Altitude
431.063 km
Speed
7.651 km/s
True Right ascension
01h 25m 39s
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
02:01:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
426.141 km
Perigee altitude
416.142 km
Semi-major axis
6,799.278 km
Eccentricity
0.00074
Inclination
97.3519°
RAAN
21.4156°
Arg. of periapsis
138.1918°
True anomaly
221.93317°
Mean anomaly
221.9895°
Eccentric anomaly
221.96133°
Mean motion
3.87123 °/min
Orbital period
92.99 mins
BSTAR
0.00086304
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Other satellites on launch #1 in the year 2023 (2023-01-03 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.SKYKRAFT-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-12 16:46:13.383Z | 44.848° NE | 2025-11-12 16:48:13.383Z | 85.146° E | 20.011° | 2025-11-12 16:50:13.383Z | 136.279° SSE |
| 5 mins | 2025-11-13 04:45:13.383Z | 179.107° S | 2025-11-13 04:47:13.383Z | 236.534° WSW | 42.041° | 2025-11-13 04:50:13.383Z | 341.408° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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