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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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: 5 hours ago
TLE from 5 hours ago
0 BOTSAT-1
1 63216U 25052G 26251.60177469 .00008830 00000-0 32211-3 0 9999
2 63216 97.3768 144.6472 0002635 143.3519 216.7901 15.28381325 82699Epoch: 2026-09-08T14:26Z
TLE epoch observation values (Epoch: 2026-09-08T14:26:33.333Z)
Latitude
-0.00005°
Longitude
-59.65752°
Altitude
485.201 km
Speed
7.622 km/s
True Right ascension
09h 38m 35s
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
11:42:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.411 km
Perigee altitude
475.798 km
Semi-major axis
6,855.741 km
Eccentricity
0.00026
Inclination
97.3768°
RAAN
144.6472°
Arg. of periapsis
143.3519°
True anomaly
216.77202°
Mean anomaly
216.7901°
Eccentric anomaly
216.78106°
Mean motion
3.8235 °/min
Orbital period
94.15 mins
BSTAR
0.00032211
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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 | 2026-09-09 05:09:35.077Z | 46.113° ENE | 2026-09-09 05:11:35.077Z | 85.644° E | 23.662° | 2026-09-09 05:14:35.077Z | 148.802° SSE |
| 5 mins | 2026-09-09 17:17:35.077Z | 190.784° SSW | 2026-09-09 17:19:35.077Z | 257.377° W | 52.696° | 2026-09-09 17:22:35.077Z | 335.889° NNW |
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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