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: 18 hours ago
TLE from 18 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 25260.27883199 .00019341 00000-0 43369-3 0 9999
2 55041 97.3616 325.7068 0006189 354.7582 5.3600 15.43433464150656Epoch: 2025-09-17T06:41Z
TLE epoch observation values (Epoch: 2025-09-17T06:41:31.083Z)
Latitude
-0.00006°
Longitude
-131.12977°
Altitude
434.908 km
Speed
7.653 km/s
True Right ascension
21h 42m 49s
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
17:43:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.133 km
Perigee altitude
428.702 km
Semi-major axis
6,811.055 km
Eccentricity
0.00062
Inclination
97.3616°
RAAN
325.7068°
Arg. of periapsis
354.7582°
True anomaly
5.36663°
Mean anomaly
5.36°
Eccentric anomaly
5.36331°
Mean motion
3.86119 °/min
Orbital period
93.24 mins
BSTAR
0.00043369
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 04:36:20.675Z | 174.774° S | 2025-09-18 04:39:20.675Z | 316.001° NNW | 40.729° | 2025-09-18 04:41:20.675Z | 342.197° N |
| 5 mins | 2025-09-18 17:29:20.675Z | 1.843° NNE | 2025-09-18 17:31:20.675Z | 299.647° NW | 41.974° | 2025-09-18 17:34:20.675Z | 202.88° SW |
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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