COSMOS 1414 (GLONASS), 13606
Orbit data source: Space-Track
COSMOS 1414 (GLONASS), 13606 is a payload satellite owned by GUKOS (CIS) in MEO that was launched on Tue, 12 Oct 1982 UTC via a PROTON-K/DM-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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13606 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Omsk Av. Zav.
Mission
Non-operational spacecraft
Bus & Motor
URAGAN, Unknown motor
Mass
1,300 kg wet, ~1,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 COSMOS 1414 (GLONASS)
1 13606U 82100D 26162.39373439 -.00000032 00000-0 00000+0 0 9990
2 13606 64.7926 71.3949 0079116 32.9136 148.5226 2.13103729339778Epoch: 2026-06-11T09:26Z
TLE epoch observation values (Epoch: 2026-06-11T09:26:58.651Z)
Latitude
-1.76431°
Longitude
-149.25238°
Altitude
19,303.399 km
Speed
3.926 km/s
True Right ascension
16h 48m 55s
True Declination
-1° 45' 41"
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
18:38:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,331.177 km
Perigee altitude
18,927.566 km
Semi-major axis
25,507.509 km
Eccentricity
0.00791
Inclination
64.7926°
RAAN
71.3949°
Arg. of periapsis
32.9136°
True anomaly
148.99203°
Mean anomaly
148.5226°
Eccentric anomaly
148.75771°
Mean motion
0.53277 °/min
Orbital period
675.71 mins
BSTAR
0
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Other satellites on launch #100 in the year 1982 (1982-10-12 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.COSMOS 1414 (GLONASS) 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. |
|---|---|---|---|---|---|---|---|
| 337 mins | 2026-06-14 00:09:32.786Z | 280.552° WNW | 2026-06-14 03:20:32.786Z | 61.313° ENE | 43.74° | 2026-06-14 05:46:32.786Z | 160.959° S |
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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