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: 14 hours ago
TLE from 14 hours ago
0 PROTOSAT-1
1 61793U 24201B 25260.73370910 .00020080 00000-0 17495-2 0 9998
2 61793 97.9106 170.6253 0006768 353.9270 6.1868 14.96908172 47041Epoch: 2025-09-17T17:36Z
TLE epoch observation values (Epoch: 2025-09-17T17:36:32.466Z)
Latitude
-0°
Longitude
-90.41539°
Altitude
574.82 km
Speed
7.576 km/s
True Right ascension
11h 22m 30s
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
00:47:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.18 km
Perigee altitude
568.77 km
Semi-major axis
6,951.612 km
Eccentricity
0.00068
Inclination
97.9106°
RAAN
170.6253°
Arg. of periapsis
353.927°
True anomaly
6.19517°
Mean anomaly
6.1868°
Eccentric anomaly
6.19098°
Mean motion
3.74468 °/min
Orbital period
96.14 mins
BSTAR
0.0017495
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 17:47:53.817Z | 149.74° SSE | 2025-09-18 17:50:53.817Z | 102.289° ESE | 37.882° | 2025-09-18 17:54:53.817Z | 358.157° N |
| 7 mins | 2025-09-19 07:03:53.817Z | 9.309° NNE | 2025-09-19 07:07:53.817Z | 241.941° WSW | 43.819° | 2025-09-19 07:10:53.817Z | 199.302° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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