PROTOSAT-1, 61793
Orbit data source: Space-Track
PROTOSAT-1, 61793 is a Rwandan payload satellite in SSO that was launched on Tue, 05 Nov 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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61793 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
RW / RWARelated business
Manufacturer
E-Space
Mission
Operational Commercial Communications
Bus & Motor
E-SPACE, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.446 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 PROTOSAT-1
1 61793U 24201B 25347.00588345 .00097851 00000-0 56905-2 0 9996
2 61793 97.9145 258.9417 0007919 23.6877 336.4715 15.11593836 60016Epoch: 2025-12-13T00:08Z
TLE epoch observation values (Epoch: 2025-12-13T00:08:28.330Z)
Latitude
-0.00002°
Longitude
174.8843°
Altitude
529.386 km
Speed
7.601 km/s
True Right ascension
17h 15m 46s
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
15:17:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.807 km
Perigee altitude
522.869 km
Semi-major axis
6,906.475 km
Eccentricity
0.00079
Inclination
97.9145°
RAAN
258.9417°
Arg. of periapsis
23.6877°
True anomaly
336.43524°
Mean anomaly
336.4715°
Eccentric anomaly
336.45337°
Mean motion
3.78145 °/min
Orbital period
95.2 mins
BSTAR
0.0056905
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Other satellites on launch #201 in the year 2024 (2024-11-05 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.PROTOSAT-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 | 2025-12-13 17:45:04.847Z | 132.565° SE | 2025-12-13 17:48:04.847Z | 71.724° E | 28.228° | 2025-12-13 17:51:04.847Z | 10.412° NNE |
| 6 mins | 2025-12-14 06:54:04.847Z | 30.297° NE | 2025-12-14 06:56:04.847Z | 72.777° E | 36.128° | 2025-12-14 07:00:04.847Z | 176.032° 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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