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: 4 hours ago
TLE from 4 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 25357.94531392 .00035462 00000-0 61197-3 0 9996
2 55041 97.3446 64.8917 0005789 2.2196 357.9080 15.50921817165759Epoch: 2025-12-23T22:41Z
TLE epoch observation values (Epoch: 2025-12-23T22:41:15.122Z)
Latitude
-0.0001°
Longitude
-8.14307°
Altitude
413.237 km
Speed
7.665 km/s
True Right ascension
04h 19m 34s
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
02:20:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
414.886 km
Perigee altitude
407.025 km
Semi-major axis
6,789.092 km
Eccentricity
0.00058
Inclination
97.3446°
RAAN
64.8917°
Arg. of periapsis
2.2196°
True anomaly
357.90558°
Mean anomaly
357.908°
Eccentric anomaly
357.90679°
Mean motion
3.87995 °/min
Orbital period
92.78 mins
BSTAR
0.00061197
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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 | 2025-12-24 05:01:00.703Z | 193.803° SSW | 2025-12-24 05:03:00.703Z | 256.731° W | 34.584° | 2025-12-24 05:06:00.703Z | 334.199° NNW |
| 4 mins | 2025-12-24 17:50:00.703Z | 350.842° N | 2025-12-24 17:52:00.703Z | 280.125° WNW | 35.369° | 2025-12-24 17:54:00.703Z | 217.991° 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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