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, 14.5 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 25347.97012643 .00012389 00000-0 52611-3 0 9996
2 63216 97.4081 238.8930 0004639 66.9274 293.2451 15.23203051 41720Epoch: 2025-12-13T23:16Z
TLE epoch observation values (Epoch: 2025-12-13T23:16:58.923Z)
Latitude
-0.00008°
Longitude
166.75774°
Altitude
498.024 km
Speed
7.616 km/s
True Right ascension
15h 55m 34s
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
08:47:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.336 km
Perigee altitude
489.961 km
Semi-major axis
6,871.285 km
Eccentricity
0.00046
Inclination
97.4081°
RAAN
238.893°
Arg. of periapsis
66.9274°
True anomaly
293.19624°
Mean anomaly
293.2451°
Eccentric anomaly
293.22067°
Mean motion
3.81054 °/min
Orbital period
94.47 mins
BSTAR
0.00052611
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-15 16:24:46.363Z | 132.287° SE | 2025-12-15 16:27:46.363Z | 61.588° ENE | 27.791° | 2025-12-15 16:29:46.363Z | 16.629° NNE |
| 5 mins | 2025-12-16 05:27:46.363Z | 31.316° NE | 2025-12-16 05:29:46.363Z | 80.914° E | 35.737° | 2025-12-16 05:32:46.363Z | 170.385° 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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