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: 1 day ago
TLE from 1 day ago
0 DJIBOUTI-1B
1 62402U 24247AB 25338.13251219 .00058212 00000-0 15173-2 0 9995
2 62402 44.9764 260.4058 0007417 127.9723 232.1835 15.38074716 53335Epoch: 2025-12-04T03:10Z
TLE epoch observation values (Epoch: 2025-12-04T03:10:49.053Z)
Latitude
0.00002°
Longitude
139.50809°
Altitude
454.907 km
Speed
7.64 km/s
True Right ascension
17h 21m 37s
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
12:58:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.49 km
Perigee altitude
448.357 km
Semi-major axis
6,831.56 km
Eccentricity
0.00074
Inclination
44.9764°
RAAN
260.4058°
Arg. of periapsis
127.9723°
True anomaly
232.1164°
Mean anomaly
232.1835°
Eccentric anomaly
232.14994°
Mean motion
3.84382 °/min
Orbital period
93.66 mins
BSTAR
0.0015173
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-05 21:27:00.870Z | 211.235° SW | 2025-12-05 21:30:00.870Z | 149.062° SSE | 29.019° | 2025-12-05 21:33:00.870Z | 82.587° E |
| 5 mins | 2025-12-05 23:06:00.870Z | 271.377° WNW | 2025-12-05 23:08:00.870Z | 339.181° N | 39.353° | 2025-12-05 23:11:00.870Z | 60.176° ENE |
| 4 mins | 2025-12-06 00:45:00.870Z | 313.692° NW | 2025-12-06 00:47:00.870Z | 20.826° NNE | 28.458° | 2025-12-06 00:49:00.870Z | 62.721° ENE |
| 5 mins | 2025-12-06 02:23:00.870Z | 303.313° NW | 2025-12-06 02:25:00.870Z | 28.064° NE | 41.953° | 2025-12-06 02:28:00.870Z | 101.164° ESE |
| 4 mins | 2025-12-06 04:01:00.870Z | 260.474° W | 2025-12-06 04:03:00.870Z | 209.645° SW | 23.939° | 2025-12-06 04:05:00.870Z | 165.332° 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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