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: 2 days ago
TLE from 2 days ago
0 CROCUBE
1 62394U 24247T 25340.11439712 .00038933 00000-0 11379-2 0 9994
2 62394 44.9746 256.5076 0003153 78.8007 281.3233 15.34700535 53556Epoch: 2025-12-06T02:44Z
TLE epoch observation values (Epoch: 2025-12-06T02:44:43.911Z)
Latitude
0.00002°
Longitude
140.17787°
Altitude
461.383 km
Speed
7.638 km/s
True Right ascension
17h 06m 01s
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
13:26:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.586 km
Perigee altitude
461.271 km
Semi-major axis
6,841.566 km
Eccentricity
0.00032
Inclination
44.9746°
RAAN
256.5076°
Arg. of periapsis
78.8007°
True anomaly
281.28787°
Mean anomaly
281.3233°
Eccentric anomaly
281.30559°
Mean motion
3.83539 °/min
Orbital period
93.86 mins
BSTAR
0.0011379
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 21:06:34.834Z | 213.623° SW | 2025-12-07 21:09:34.834Z | 154.282° SSE | 30.306° | 2025-12-07 21:12:34.834Z | 82.649° E |
| 5 mins | 2025-12-07 22:45:34.834Z | 270.23° WNW | 2025-12-07 22:47:34.834Z | 315.01° NNW | 37.561° | 2025-12-07 22:50:34.834Z | 57.914° ENE |
| 5 mins | 2025-12-08 00:24:34.834Z | 304.831° NW | 2025-12-08 00:26:34.834Z | 357.426° N | 30.011° | 2025-12-08 00:29:34.834Z | 66.986° ENE |
| 5 mins | 2025-12-08 02:03:34.834Z | 303.469° NW | 2025-12-08 02:05:34.834Z | 50.511° ENE | 42.108° | 2025-12-08 02:08:34.834Z | 103.367° ESE |
| 4 mins | 2025-12-08 03:41:34.834Z | 259.741° W | 2025-12-08 03:43:34.834Z | 211.548° SW | 23.227° | 2025-12-08 03:45:34.834Z | 168.14° S |
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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