BOTSAT-1, 63216
Orbit data source: Space-Track
BOTSAT-1, 63216 is a Batswana payload satellite in SSO that was launched on Sat, 15 Mar 2025 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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63216 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
BW / BWARelated business
Manufacturer
Endurosat
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BOTSAT-1
1 63216U 25052G 25257.69374700 .00007016 00000-0 32349-3 0 9997
2 63216 97.4142 149.9584 0004159 47.7795 312.3793 15.20557540 27994Epoch: 2025-09-14T16:38Z
TLE epoch observation values (Epoch: 2025-09-14T16:38:59.74Z)
Latitude
-0.00002°
Longitude
-93.6996°
Altitude
505.32 km
Speed
7.613 km/s
True Right ascension
09h 59m 50s
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
12:16:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.984 km
Perigee altitude
498.262 km
Semi-major axis
6,879.26 km
Eccentricity
0.00042
Inclination
97.4142°
RAAN
149.9584°
Arg. of periapsis
47.7795°
True anomaly
312.34408°
Mean anomaly
312.3793°
Eccentric anomaly
312.36169°
Mean motion
3.80391 °/min
Orbital period
94.64 mins
BSTAR
0.00032349
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.BOTSAT-1 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 | 2025-09-16 05:32:05.788Z | 21.635° NNE | 2025-09-16 05:35:05.788Z | 78.54° E | 39.295° | 2025-09-16 05:38:05.788Z | 176.288° S |
| 4 mins | 2025-09-16 17:45:05.788Z | 228.266° WSW | 2025-09-16 17:47:05.788Z | 271.748° WNW | 19.756° | 2025-09-16 17:49:05.788Z | 309.665° NW |
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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