COSMOS 1415 (GLONASS), 13607
Orbit data source: Space-Track
COSMOS 1415 (GLONASS), 13607 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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13607 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 COSMOS 1415 (GLONASS)
1 13607U 82100E 26090.66172037 -.00000002 00000-0 00000-0 0 9990
2 13607 64.8165 69.4937 0005052 22.9265 191.7075 2.13810137339286Epoch: 2026-03-31T15:52Z
TLE epoch observation values (Epoch: 2026-03-31T15:52:52.639Z)
Latitude
-31.03655°
Longitude
-161.35777°
Altitude
19,095.956 km
Speed
3.955 km/s
True Right ascension
17h 43m 35s
True Declination
-30° 59' 39"
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
14:56:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,086.013 km
Perigee altitude
19,060.297 km
Semi-major axis
25,451.292 km
Eccentricity
0.00051
Inclination
64.8165°
RAAN
69.4937°
Arg. of periapsis
22.9265°
True anomaly
191.69576°
Mean anomaly
191.7075°
Eccentric anomaly
191.70163°
Mean motion
0.53454 °/min
Orbital period
673.48 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 1415 (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. |
|---|---|---|---|---|---|---|---|
| 242 mins | 2026-04-09 08:46:28.809Z | 325.79° NNW | 2026-04-09 10:42:28.809Z | 275.165° WNW | 41.784° | 2026-04-09 12:48:28.809Z | 205.779° SW |
| 137 mins | 2026-04-09 18:13:28.809Z | 90.082° ESE | 2026-04-09 19:23:28.809Z | 54.664° ENE | 21.547° | 2026-04-09 20:30:28.809Z | 23.978° NE |
| 135 mins | 2026-04-10 06:31:28.809Z | 309.316° NW | 2026-04-10 08:46:28.809Z | 328.8° NNW | 44.135° | 2026-04-10 08:46:28.809Z | 328.8° NNW |
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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