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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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/55041?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/55041?theme=dark&initialShowStats=false

Optional secondary NORAD IDs

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ISO8601 Format

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ISO8601 Format

Identifier

55041, 2023-001AJ

Orbit

SSO

Country

AU / AUS

Related business

Manufacturer

SkyKraft

Mission

Operational Commercial Technology

Bus & Motor

SKYKRAFT CARRIER, AOCS

Mass

~100 kg wet, ~100 kg dry

Launch date (UTC)

2023-01-03 (4 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.3 m

Radar Cross Section

0.065 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago

0 SKYKRAFT-1
1 55041U 23001AJ  26313.27546611  .00241256  23439-4  77751-3 0  9993
2 55041  97.3029  38.4026 0002789 239.9619 120.1378 15.90894255215902

Epoch: 2026-11-09T06:36Z

TLE epoch observation values (Epoch: 2026-11-09T06:36:40.271Z)

Latitude

-0.00007°

Longitude

-109.21954°

Altitude

303.904 km

Speed

7.725 km/s

True Right ascension

02h 33m 36s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

16:15:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

298.508 km

Perigee altitude

294.785 km

Semi-major axis

6,674.784 km

Eccentricity

0.00028

Inclination

97.3029°

RAAN

38.4026°

Arg. of periapsis

239.9619°

True anomaly

120.16543°

Mean anomaly

120.1378°

Eccentric anomaly

120.15162°

Mean motion

3.98004 °/min

Orbital period

90.45 mins

BSTAR

0.00077751

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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)

LEMUR 2 STEVEALBERS, 55017 (Decayed)

ASTROCAST-0402, 55109

ASTROCAST-0401, 55110

ASTROCAST-0403, 55111

ASTROCAST-0404, 55112

SHARJAHSAT-1, 55104

KUWAITSAT-1, 55103

SKYKRAFT-1C, 55061

ION SCV-007, 55060

ION SCV-008, 55051

EOSSAT-1, 55053

SKYKRAFT-1A, 55054

VIGORIDE 5, 55056

CONTINUUM-1, 55045

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

SKYKRAFT-1 Visibility

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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.
SKYKRAFT-1 is likely not visible in the next few days.

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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Check out SKYKRAFT-1, 55041 on other resources

View SKYKRAFT-1, 55041 on NASA - NSSDCA Website

View SKYKRAFT-1, 55041 on Heavens-Above

View SKYKRAFT-1, 55041 on Keep Track

View SKYKRAFT-1, 55041 on Celestrak

View SKYKRAFT-1, 55041 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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