PERUSAT 1, 41770
Orbit data source: Space-Track
PERUSAT 1, 41770 is a payload satellite owned by MOD Peru (PE) in SSO that was launched on Fri, 16 Sep 2016 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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41770 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PE / PERRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Defense Imaging
Bus & Motor
ASTROBUS-S, Unknown motor
Mass
430 kg wet, ~400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 3 Pan, 2.6 m
Radar Cross Section
3.025 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 PERUSAT 1
1 41770U 16058A 25290.79816125 .00000794 00000-0 18066-3 0 9990
2 41770 98.1772 2.8441 0001339 87.6610 272.4742 14.58531522483760Epoch: 2025-10-17T19:09Z
TLE epoch observation values (Epoch: 2025-10-17T19:09:21.132Z)
Latitude
-0.00006°
Longitude
48.96769°
Altitude
700.863 km
Speed
7.506 km/s
True Right ascension
00h 11m 22s
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
19:27:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
695.949 km
Perigee altitude
694.055 km
Semi-major axis
7,073.139 km
Eccentricity
0.00013
Inclination
98.1772°
RAAN
2.8441°
Arg. of periapsis
87.661°
True anomaly
272.45887°
Mean anomaly
272.4742°
Eccentric anomaly
272.46654°
Mean motion
3.64859 °/min
Orbital period
98.67 mins
BSTAR
0.00018066
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Other satellites on launch #58 in the year 2016 (2016-09-16 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.PERUSAT 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-18 05:09:27.714Z | 180.298° SSW | 2025-10-18 05:13:27.714Z | 291.816° WNW | 40.586° | 2025-10-18 05:17:27.714Z | 340.145° N |
| 7 mins | 2025-10-18 17:09:27.714Z | 43.699° NE | 2025-10-18 17:12:27.714Z | 102.882° ESE | 28.718° | 2025-10-18 17:16:27.714Z | 161.608° S |
| 5 mins | 2025-10-18 18:47:27.714Z | 331.58° NNW | 2025-10-18 18:49:27.714Z | 298.078° NW | 22.318° | 2025-10-18 18:52:27.714Z | 248.554° W |
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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