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: 5 hours ago
TLE from 5 hours ago
0 PERUSAT 1
1 41770U 16058A 25307.81151781 .00000479 00000-0 11286-3 0 9999
2 41770 98.1752 19.5810 0001231 89.2555 270.8786 14.58553298486240Epoch: 2025-11-03T19:28Z
TLE epoch observation values (Epoch: 2025-11-03T19:28:35.138Z)
Latitude
0.00002°
Longitude
44.12705°
Altitude
700.82 km
Speed
7.506 km/s
True Right ascension
01h 18m 19s
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
20:25:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
695.802 km
Perigee altitude
694.06 km
Semi-major axis
7,073.068 km
Eccentricity
0.00012
Inclination
98.1752°
RAAN
19.581°
Arg. of periapsis
89.2555°
True anomaly
270.8645°
Mean anomaly
270.8786°
Eccentric anomaly
270.87155°
Mean motion
3.64864 °/min
Orbital period
98.67 mins
BSTAR
0.00011286
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-04 03:51:21.423Z | 112.385° ESE | 2025-11-04 03:54:21.423Z | 71.226° E | 19.654° | 2025-11-04 03:57:21.423Z | 25.174° NE |
| 7 mins | 2025-11-04 05:29:21.423Z | 204.519° SW | 2025-11-04 05:32:21.423Z | 272.685° WNW | 32.058° | 2025-11-04 05:36:21.423Z | 330.926° NNW |
| 7 mins | 2025-11-04 17:28:21.423Z | 30.281° NE | 2025-11-04 17:31:21.423Z | 102.484° ESE | 38.648° | 2025-11-04 17:35:21.423Z | 175.567° S |
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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