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: 8 hours ago
TLE from 8 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 26035.47570921 .00046787 00000-0 69791-3 0 9999
2 55041 97.3354 108.3862 0005261 189.8437 170.2715 15.54925418172355Epoch: 2026-02-04T11:25Z
TLE epoch observation values (Epoch: 2026-02-04T11:25:01.275Z)
Latitude
-0.00004°
Longitude
162.48914°
Altitude
409.026 km
Speed
7.663 km/s
True Right ascension
07h 13m 32s
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
21:37:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
402.851 km
Perigee altitude
395.72 km
Semi-major axis
6,777.423 km
Eccentricity
0.00053
Inclination
97.3354°
RAAN
108.3862°
Arg. of periapsis
189.8437°
True anomaly
170.28168°
Mean anomaly
170.2715°
Eccentric anomaly
170.27659°
Mean motion
3.88997 °/min
Orbital period
92.55 mins
BSTAR
0.00069791
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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 | 2026-02-05 04:32:32.455Z | 146.967° SSE | 2026-02-05 04:34:32.455Z | 100.857° ESE | 35.223° | 2026-02-05 04:37:32.455Z | 1.654° NNE |
| 4 mins | 2026-02-05 17:20:32.455Z | 44.704° NE | 2026-02-05 17:21:32.455Z | 83.42° E | 33.683° | 2026-02-05 17:24:32.455Z | 171.89° S |
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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