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, 0.087 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 CROCUBE
1 62394U 24247T 26282.57311726 .00059790 00000-0 80053-3 0 9994
2 62394 44.9699 330.7993 0009832 0.3389 359.7510 15.57170897101121Epoch: 2026-10-09T13:45Z
TLE epoch observation values (Epoch: 2026-10-09T13:45:17.331Z)
Latitude
-0.00001°
Longitude
106.28441°
Altitude
389.185 km
Speed
7.682 km/s
True Right ascension
22h 03m 11s
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
02:53:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.146 km
Perigee altitude
390.823 km
Semi-major axis
6,775.621 km
Eccentricity
0.00098
Inclination
44.9699°
RAAN
330.7993°
Arg. of periapsis
0.3389°
True anomaly
359.75051°
Mean anomaly
359.751°
Eccentric anomaly
359.75075°
Mean motion
3.89152 °/min
Orbital period
92.51 mins
BSTAR
0.00080053
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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 | 2026-10-10 10:08:50.182Z | 304.271° NW | 2026-10-10 10:10:50.182Z | 347.175° N | 32.47° | 2026-10-10 10:13:50.182Z | 72.253° E |
| 4 mins | 2026-10-10 11:46:50.182Z | 289.252° WNW | 2026-10-10 11:48:50.182Z | 133.159° SE | 59.964° | 2026-10-10 11:50:50.182Z | 119.443° SE |
| 4 mins | 2026-10-11 05:59:50.182Z | 199.387° SSW | 2026-10-11 06:00:50.182Z | 170.075° S | 33.565° | 2026-10-11 06:03:50.182Z | 82.756° E |
| 4 mins | 2026-10-11 07:36:50.182Z | 286.972° WNW | 2026-10-11 07:37:50.182Z | 326.8° NNW | 45.703° | 2026-10-11 07:40:50.182Z | 58.251° ENE |
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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