PROTOSAT-1, 61793 (Decayed)
Orbit data source: Space-Track
PROTOSAT-1, 61793 was a Rwandan payload satellite in LEO 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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Identifier
Orbit
Country
RW / RWARelated business
Manufacturer
E-Space
Mission
Decayed 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: 3 weeks ago
TLE from 3 weeks ago
0 PROTOSAT-1
1 61793U 24201B 26054.82519766 .00032486 00000-0 11844-2 0 9999
2 61793 43.0012 257.7765 0001473 278.2072 81.8612 15.27591600 72764Epoch: 2026-02-23T19:48Z
TLE epoch observation values (Epoch: 2026-02-23T19:48:17.077Z)
Latitude
-0.00007°
Longitude
166.99175°
Altitude
482.647 km
Speed
7.626 km/s
True Right ascension
17h 11m 06s
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
02:56:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.97 km
Perigee altitude
483.948 km
Semi-major axis
6,863.096 km
Eccentricity
0.00015
Inclination
43.0012°
RAAN
257.7765°
Arg. of periapsis
278.2072°
True anomaly
81.87791°
Mean anomaly
81.8612°
Eccentric anomaly
81.86955°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.0011844
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-14 07:54:35.873Z | 175.639° S | 2026-03-14 07:56:35.873Z | 140.33° SSE | 15.223° | 2026-03-14 07:58:35.873Z | 106.43° ESE |
| 5 mins | 2026-03-14 09:32:35.873Z | 237.671° WSW | 2026-03-14 09:34:35.873Z | 195.709° SSW | 42.239° | 2026-03-14 09:37:35.873Z | 76.315° E |
| 5 mins | 2026-03-14 11:11:35.873Z | 283.992° WNW | 2026-03-14 11:13:35.873Z | 335.798° NNW | 38.045° | 2026-03-14 11:16:35.873Z | 69.149° E |
| 6 mins | 2026-03-14 12:50:35.873Z | 293.11° NW | 2026-03-14 12:52:35.873Z | 331.112° NNW | 41.177° | 2026-03-14 12:56:35.873Z | 96.682° ESE |
| 5 mins | 2026-03-14 14:29:35.873Z | 266.574° W | 2026-03-14 14:31:35.873Z | 215.815° SW | 30.661° | 2026-03-14 14:34:35.873Z | 145.694° SSE |
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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