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: 11 hours ago
TLE from 11 hours ago
0 SKYKRAFT-1
1 55041U 23001AJ 25258.33379050 .00035500 00000-0 79472-3 0 9998
2 55041 97.3613 323.7405 0006375 2.5805 357.5474 15.43359685150359Epoch: 2025-09-15T08:00Z
TLE epoch observation values (Epoch: 2025-09-15T08:00:39.499Z)
Latitude
-0.00007°
Longitude
-150.96401°
Altitude
434.984 km
Speed
7.653 km/s
True Right ascension
21h 34m 57s
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
11:41:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.477 km
Perigee altitude
428.793 km
Semi-major axis
6,811.272 km
Eccentricity
0.00064
Inclination
97.3613°
RAAN
323.7405°
Arg. of periapsis
2.5805°
True anomaly
357.54427°
Mean anomaly
357.5474°
Eccentric anomaly
357.54584°
Mean motion
3.86101 °/min
Orbital period
93.24 mins
BSTAR
0.00079472
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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 | 2025-09-16 04:22:37.587Z | 156.59° SSE | 2025-09-16 04:24:37.587Z | 108.417° ESE | 42.076° | 2025-09-16 04:27:37.587Z | 354.486° N |
| 5 mins | 2025-09-16 17:15:37.587Z | 18.415° NNE | 2025-09-16 17:17:37.587Z | 136.496° SSE | 43.81° | 2025-09-16 17:20:37.587Z | 188.023° SSW |
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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