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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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 26093.00483506 .00061621 00000-0 13546-2 0 9996
2 62394 44.9742 321.5870 0004821 230.0636 129.9829 15.43212573 71716Epoch: 2026-04-03T00:06Z
TLE epoch observation values (Epoch: 2026-04-03T00:06:57.749Z)
Latitude
-0.00003°
Longitude
128.50116°
Altitude
438.743 km
Speed
7.649 km/s
True Right ascension
21h 26m 20s
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
18:22:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.546 km
Perigee altitude
434.973 km
Semi-major axis
6,816.397 km
Eccentricity
0.00048
Inclination
44.9742°
RAAN
321.587°
Arg. of periapsis
230.0636°
True anomaly
130.02521°
Mean anomaly
129.9829°
Eccentric anomaly
130.00406°
Mean motion
3.85666 °/min
Orbital period
93.35 mins
BSTAR
0.0013546
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Other satellites on launch #247 in the year 2024 (2024-12-21 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.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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-04 18:17:29.068Z | 227.464° WSW | 2026-04-04 18:19:29.068Z | 136.855° SSE | 41.706° | 2026-04-04 18:22:29.068Z | 71.472° E |
| 5 mins | 2026-04-04 19:55:29.068Z | 292.549° NW | 2026-04-04 19:57:29.068Z | 2.806° NNE | 32.327° | 2026-04-04 20:00:29.068Z | 61.175° ENE |
| 5 mins | 2026-04-04 21:33:29.068Z | 310.633° NW | 2026-04-04 21:35:29.068Z | 12.175° NNE | 31.297° | 2026-04-04 21:38:29.068Z | 77.08° E |
| 5 mins | 2026-04-04 23:11:29.068Z | 288.878° WNW | 2026-04-04 23:13:29.068Z | 169.09° S | 44.015° | 2026-04-04 23:16:29.068Z | 120.016° SE |
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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