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: 10 hours ago
TLE from 10 hours ago
0 PROTOSAT-1
1 61793U 24201B 25346.27768859 .00100693 00000-0 58726-2 0 9996
2 61793 97.9141 258.1889 0008261 27.1725 332.9935 15.11472659 59909Epoch: 2025-12-12T06:39Z
TLE epoch observation values (Epoch: 2025-12-12T06:39:52.294Z)
Latitude
0.00002°
Longitude
76.99939°
Altitude
529.686 km
Speed
7.601 km/s
True Right ascension
17h 12m 45s
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
15:10:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.413 km
Perigee altitude
523.002 km
Semi-major axis
6,906.845 km
Eccentricity
0.00083
Inclination
97.9141°
RAAN
258.1889°
Arg. of periapsis
27.1725°
True anomaly
332.95047°
Mean anomaly
332.9935°
Eccentric anomaly
332.97199°
Mean motion
3.78115 °/min
Orbital period
95.21 mins
BSTAR
0.0058726
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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 | 2025-12-12 17:55:27.925Z | 139.329° SSE | 2025-12-12 17:58:27.925Z | 56.519° ENE | 33.863° | 2025-12-12 18:01:27.925Z | 2.415° NNE |
| 6 mins | 2025-12-13 07:04:27.925Z | 21.845° NNE | 2025-12-13 07:06:27.925Z | 68.799° E | 42.536° | 2025-12-13 07:10:27.925Z | 186.072° SSW |
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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