DJIBOUTI-1B, 62402
Orbit data source: Space-Track
DJIBOUTI-1B, 62402 is a Djibouti 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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62402 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DJ / DJIRelated business
Manufacturer
Montpellier
Mission
Operational Civil 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: 14 hours ago
TLE from 14 hours ago
0 DJIBOUTI-1B
1 62402U 24247AB 25297.88875037 .00034065 00000-0 98938-3 0 9992
2 62402 44.9758 123.1892 0008852 228.6956 131.3168 15.34924927 47145Epoch: 2025-10-24T21:19Z
TLE epoch observation values (Epoch: 2025-10-24T21:19:48.031Z)
Latitude
-0.00004°
Longitude
129.71184°
Altitude
465.139 km
Speed
7.633 km/s
True Right ascension
08h 12m 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
06:14:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.817 km
Perigee altitude
456.706 km
Semi-major axis
6,840.899 km
Eccentricity
0.00089
Inclination
44.9758°
RAAN
123.1892°
Arg. of periapsis
228.6956°
True anomaly
131.39293°
Mean anomaly
131.3168°
Eccentric anomaly
131.35487°
Mean motion
3.83595 °/min
Orbital period
93.85 mins
BSTAR
0.00098938
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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.DJIBOUTI-1B 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 | 2025-10-25 14:41:18.669Z | 174.897° S | 2025-10-25 14:43:18.669Z | 138.262° SSE | 15.923° | 2025-10-25 14:45:18.669Z | 102.828° ESE |
| 5 mins | 2025-10-25 16:19:18.669Z | 242.471° WSW | 2025-10-25 16:21:18.669Z | 90.067° ESE | 44.533° | 2025-10-25 16:24:18.669Z | 67.272° ENE |
| 5 mins | 2025-10-25 17:57:18.669Z | 291.249° WNW | 2025-10-25 17:59:18.669Z | 337.584° N | 31.035° | 2025-10-25 18:02:18.669Z | 57.715° ENE |
| 5 mins | 2025-10-25 19:36:18.669Z | 308.36° NW | 2025-10-25 19:38:18.669Z | 6.13° NNE | 34.523° | 2025-10-25 19:41:18.669Z | 82.06° E |
| 6 mins | 2025-10-25 21:14:18.669Z | 283.595° WNW | 2025-10-25 21:16:18.669Z | 245.188° WSW | 37.845° | 2025-10-25 21:20:18.669Z | 130.248° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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