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: 2 days ago
TLE from 2 days ago
0 DJIBOUTI-1B
1 62402U 24247AB 25348.00149593 .00032769 00000-0 83579-3 0 9998
2 62402 44.9745 205.6027 0008877 193.2401 166.8254 15.38968522 54854Epoch: 2025-12-14T00:02Z
TLE epoch observation values (Epoch: 2025-12-14T00:02:09.248Z)
Latitude
-0.00003°
Longitude
122.14346°
Altitude
455.055 km
Speed
7.638 km/s
True Right ascension
13h 42m 24s
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
13:22:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.842 km
Perigee altitude
444.718 km
Semi-major axis
6,828.917 km
Eccentricity
0.00089
Inclination
44.9745°
RAAN
205.6027°
Arg. of periapsis
193.2401°
True anomaly
166.84856°
Mean anomaly
166.8254°
Eccentric anomaly
166.83698°
Mean motion
3.84605 °/min
Orbital period
93.6 mins
BSTAR
0.00083579
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Other satellites on launch #247 in the year 2024 (2024-12-21 UTC)
Did you know?
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 | 2025-12-15 16:43:11.536Z | 186.897° SSW | 2025-12-15 16:45:11.536Z | 148.006° SSE | 19.656° | 2025-12-15 16:47:11.536Z | 104.089° ESE |
| 5 mins | 2025-12-15 18:21:11.536Z | 254.101° W | 2025-12-15 18:23:11.536Z | 345.245° N | 44.317° | 2025-12-15 18:26:11.536Z | 64.225° ENE |
| 5 mins | 2025-12-15 19:59:11.536Z | 296.044° NW | 2025-12-15 20:01:11.536Z | 343.719° N | 29.775° | 2025-12-15 20:04:11.536Z | 59.967° ENE |
| 5 mins | 2025-12-15 21:38:11.536Z | 311.509° NW | 2025-12-15 21:40:11.536Z | 30.495° NE | 36.056° | 2025-12-15 21:43:11.536Z | 89.757° E |
| 5 mins | 2025-12-15 23:16:11.536Z | 270.659° WNW | 2025-12-15 23:18:11.536Z | 198.416° SSW | 34.104° | 2025-12-15 23:21:11.536Z | 139.306° 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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