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, 2.3 m
Radar Cross Section
3.025 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 PERUSAT 1
1 41770U 16058A 25258.96734672 .00000308 00000-0 76063-4 0 9992
2 41770 98.1807 331.5186 0001414 96.9767 263.1594 14.58553017479127Epoch: 2025-09-15T23:12Z
TLE epoch observation values (Epoch: 2025-09-15T23:12:58.756Z)
Latitude
0.00005°
Longitude
-11.89063°
Altitude
700.953 km
Speed
7.505 km/s
True Right ascension
22h 06m 04s
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
01:49:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
695.932 km
Perigee altitude
693.932 km
Semi-major axis
7,073.069 km
Eccentricity
0.00014
Inclination
98.1807°
RAAN
331.5186°
Arg. of periapsis
96.9767°
True anomaly
263.14331°
Mean anomaly
263.1594°
Eccentric anomaly
263.15136°
Mean motion
3.64864 °/min
Orbital period
98.67 mins
BSTAR
0.000076063
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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 | 2025-09-16 17:53:37.452Z | 10.593° NNE | 2025-09-16 17:57:37.452Z | 328.086° NNW | 44.421° | 2025-09-16 18:01:37.452Z | 198.186° SSW |
| 8 mins | 2025-09-17 04:58:37.452Z | 169.613° S | 2025-09-17 05:02:37.452Z | 324.805° NNW | 43.44° | 2025-09-17 05:06:37.452Z | 345.345° N |
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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