SKYKRAFT-1C, 55061
Orbit data source: Space-Track
SKYKRAFT-1C, 55061 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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55061 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
SkyKraft
Mission
Operational Commercial Communications
Bus & Motor
SKYKRAFT, Unknown motor
Mass
~50 kg wet, ~50 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-1C
1 55061U 23001BE 25286.59820516 .00005334 00000-0 23045-3 0 9994
2 55061 97.3583 340.4972 0009480 299.9130 60.1165 15.22869118153929Epoch: 2025-10-13T14:21Z
TLE epoch observation values (Epoch: 2025-10-13T14:21:24.925Z)
Latitude
-0.00001°
Longitude
102.74466°
Altitude
497.044 km
Speed
7.618 km/s
True Right ascension
22h 41m 59s
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
02:30:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.666 km
Perigee altitude
487.637 km
Semi-major axis
6,872.288 km
Eccentricity
0.00095
Inclination
97.3583°
RAAN
340.4972°
Arg. of periapsis
299.913°
True anomaly
60.21074°
Mean anomaly
60.1165°
Eccentric anomaly
60.16362°
Mean motion
3.8097 °/min
Orbital period
94.5 mins
BSTAR
0.00023045
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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-1C 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 16:09:10.634Z | 29.836° NE | 2025-10-14 16:12:10.634Z | 94.504° ESE | 32.524° | 2025-10-14 16:15:10.634Z | 165.768° S |
| 4 mins | 2025-10-15 04:21:10.634Z | 224.499° SW | 2025-10-15 04:22:10.634Z | 251.44° W | 26.177° | 2025-10-15 04:25:10.634Z | 320.826° NNW |
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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