TELEOS 1, 41169 (Decayed)
Orbit data source: Space-Track
TELEOS 1, 41169 was a payload satellite owned by AgilSpace (SG) in LEO that was launched on Wed, 16 Dec 2015 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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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41169 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SINGRelated business
Manufacturer
STE Sat Sys
Mission
Decayed Commercial Imaging
Bus & Motor
SS-400, Unknown motor
Mass
400 kg wet, 400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 4 Pan, 2.0 m
Radar Cross Section
5.312 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 TELEOS 1
1 41169U 15077D 25177.62803816 .04978187 -27512-4 80740-3 0 9995
2 41169 14.9820 136.7861 0000764 246.8638 291.1774 16.32314160529153Epoch: 2025-06-26T15:04Z
TLE epoch observation values (Epoch: 2025-06-26T15:04:22.497Z)
Latitude
0.50261°
Longitude
173.83211°
Altitude
183.191 km
Speed
7.8 km/s
True Right ascension
20h 59m 40s
True Declination
0° 29' 58"
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
12:07:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
192.875 km
Perigee altitude
191.871 km
Semi-major axis
6,570.51 km
Eccentricity
0.00008
Inclination
14.982°
RAAN
136.7861°
Arg. of periapsis
246.8638°
True anomaly
291.16924°
Mean anomaly
291.1774°
Eccentric anomaly
291.17332°
Mean motion
4.07516 °/min
Orbital period
88.34 mins
BSTAR
0.0008074
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Other satellites on launch #77 in the year 2015 (2015-12-16 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.TELEOS 1 Visibility
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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. |
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| This satellite is decayed. |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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