ASTROCAST-0404, 55112
Orbit data source: Space-Track
ASTROCAST-0404, 55112 is a payload satellite owned by Astrocast (CH) 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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55112 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SWTZRelated business
Manufacturer
Astrocast
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.5 kg wet, 4.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ASTROCAST-0404
1 55112U 23001DH 25286.68435918 .00009633 00000-0 41036-3 0 9995
2 55112 97.5775 12.7763 0008585 138.2127 221.9766 15.23147454106941Epoch: 2025-10-13T16:25Z
TLE epoch observation values (Epoch: 2025-10-13T16:25:28.633Z)
Latitude
-0.00003°
Longitude
103.92339°
Altitude
503.834 km
Speed
7.61 km/s
True Right ascension
00h 51m 06s
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
02:54:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.222 km
Perigee altitude
487.424 km
Semi-major axis
6,871.46 km
Eccentricity
0.00086
Inclination
97.5775°
RAAN
12.7763°
Arg. of periapsis
138.2127°
True anomaly
221.91086°
Mean anomaly
221.9766°
Eccentric anomaly
221.94372°
Mean motion
3.81039 °/min
Orbital period
94.48 mins
BSTAR
0.00041036
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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.ASTROCAST-0404 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 18:13:02.723Z | 34.483° NE | 2025-10-14 18:16:02.723Z | 98.8° ESE | 28.299° | 2025-10-14 18:19:02.723Z | 161.49° S |
| 5 mins | 2025-10-15 06:24:02.723Z | 206.124° SW | 2025-10-15 06:26:02.723Z | 256.287° W | 29.266° | 2025-10-15 06:29:02.723Z | 325.271° 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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