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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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: 17 hours ago
TLE from 17 hours ago
0 SKYKRAFT-1C
1 55061U 23001BE 26115.11490878 .00002791 00000-0 11574-3 0 9996
2 55061 97.3239 169.9454 0009797 343.0692 17.0217 15.24663451183398Epoch: 2026-04-25T02:45Z
TLE epoch observation values (Epoch: 2026-04-25T02:45:28.118Z)
Latitude
-0.00008°
Longitude
-84.55967°
Altitude
488.459 km
Speed
7.624 km/s
True Right ascension
11h 19m 46s
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
03:07:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.48 km
Perigee altitude
482.025 km
Semi-major axis
6,866.889 km
Eccentricity
0.00098
Inclination
97.3239°
RAAN
169.9454°
Arg. of periapsis
343.0692°
True anomaly
17.0546°
Mean anomaly
17.0217°
Eccentric anomaly
17.03815°
Mean motion
3.8142 °/min
Orbital period
94.38 mins
BSTAR
0.00011574
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-26 04:06:21.496Z | 209.869° SW | 2026-04-26 04:08:21.496Z | 282.162° WNW | 31.303° | 2026-04-26 04:10:21.496Z | 325.575° NNW |
| 4 mins | 2026-04-26 17:08:21.496Z | 326.469° NNW | 2026-04-26 17:09:21.496Z | 301.627° NW | 24.603° | 2026-04-26 17:12:21.496Z | 233.784° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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