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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CROCUBE
1 62394U 24247T 26170.49048578 .00032668 00000-0 60622-3 0 9998
2 62394 44.9701 246.5654 0007741 349.0739 10.9982 15.48397693 83709Epoch: 2026-06-19T11:46Z
TLE epoch observation values (Epoch: 2026-06-19T11:46:17.971Z)
Latitude
-0.00004°
Longitude
162.27177°
Altitude
416.242 km
Speed
7.666 km/s
True Right ascension
16h 26m 15s
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
07:19:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.306 km
Perigee altitude
417.777 km
Semi-major axis
6,801.179 km
Eccentricity
0.00077
Inclination
44.9701°
RAAN
246.5654°
Arg. of periapsis
349.0739°
True anomaly
11.01514°
Mean anomaly
10.9982°
Eccentric anomaly
11.00667°
Mean motion
3.86961 °/min
Orbital period
93.03 mins
BSTAR
0.00060622
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 07:18:50.007Z | 194.575° SSW | 2026-06-21 07:20:50.007Z | 149.718° SSE | 22.78° | 2026-06-21 07:22:50.007Z | 99.025° ESE |
| 4 mins | 2026-06-21 08:56:50.007Z | 268.987° W | 2026-06-21 08:57:50.007Z | 301.665° NW | 40.085° | 2026-06-21 09:00:50.007Z | 60.716° ENE |
| 4 mins | 2026-06-21 10:34:50.007Z | 319.367° NNW | 2026-06-21 10:35:50.007Z | 353.74° N | 28.51° | 2026-06-21 10:38:50.007Z | 63.647° ENE |
| 5 mins | 2026-06-21 12:11:50.007Z | 307.225° NW | 2026-06-21 12:13:50.007Z | 24.578° NE | 38.322° | 2026-06-21 12:16:50.007Z | 94.297° ESE |
| 4 mins | 2026-06-21 13:49:50.007Z | 255.106° W | 2026-06-21 13:50:50.007Z | 222.39° SW | 28.718° | 2026-06-21 13:53:50.007Z | 149.295° 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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