CROCUBE, 62394
Orbit data source: Space-Track
CROCUBE, 62394 is a Croatian payload satellite in LEO that was launched on Sat, 21 Dec 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62394 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
HR / HRVRelated business
Manufacturer
SpaceManic
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 CROCUBE
1 62394U 24247T 25345.06065254 .00037869 00000-0 10943-2 0 9992
2 62394 44.9747 229.1913 0003190 125.2174 234.9011 15.35069533 54316Epoch: 2025-12-11T01:27Z
TLE epoch observation values (Epoch: 2025-12-11T01:27:20.379Z)
Latitude
0.00002°
Longitude
127.33436°
Altitude
461.964 km
Speed
7.637 km/s
True Right ascension
15h 16m 45s
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
13:09:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.515 km
Perigee altitude
460.151 km
Semi-major axis
6,840.47 km
Eccentricity
0.00032
Inclination
44.9747°
RAAN
229.1913°
Arg. of periapsis
125.2174°
True anomaly
234.8712°
Mean anomaly
234.9011°
Eccentric anomaly
234.88615°
Mean motion
3.83632 °/min
Orbital period
93.84 mins
BSTAR
0.0010943
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Other satellites on launch #247 in the year 2024 (2024-12-21 UTC)
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.CROCUBE 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 | 2025-12-11 18:49:09.200Z | 178.996° S | 2025-12-11 18:51:09.200Z | 138.514° SSE | 18.277° | 2025-12-11 18:53:09.200Z | 100.331° ESE |
| 5 mins | 2025-12-11 20:27:09.200Z | 250.301° W | 2025-12-11 20:29:09.200Z | 31.331° NE | 44.476° | 2025-12-11 20:32:09.200Z | 65.393° ENE |
| 4 mins | 2025-12-11 22:06:09.200Z | 308.504° NW | 2025-12-11 22:07:09.200Z | 338.481° N | 29.989° | 2025-12-11 22:10:09.200Z | 58.378° ENE |
| 5 mins | 2025-12-11 23:44:09.200Z | 307.671° NW | 2025-12-11 23:46:09.200Z | 6.945° NNE | 35.835° | 2025-12-11 23:49:09.200Z | 85.717° E |
| 5 mins | 2025-12-12 01:22:09.200Z | 279.652° WNW | 2025-12-12 01:24:09.200Z | 235.394° WSW | 35.265° | 2025-12-12 01:27:09.200Z | 140.329° SSE |
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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