OBJECT E, 45915
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT E, 45915 is a satellite owned by TsNIIKhM (CIS) in SSO that was launched on Mon, 25 Nov 2019 UTC via a SOYUZ-2-1V launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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45915 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TsNIIKhM
Mission
Defense Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OBJECT E
1 45915U 19079E 25260.98161289 .00002067 00000-0 19479-3 0 9997
2 45915 97.6694 270.6053 0174461 163.6311 197.0639 14.84066848279253Epoch: 2025-09-17T23:33Z
TLE epoch observation values (Epoch: 2025-09-17T23:33:31.353Z)
Latitude
-0.00002°
Longitude
-79.9251°
Altitude
736.413 km
Speed
7.424 km/s
True Right ascension
18h 02m 25s
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
00:23:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
735.518 km
Perigee altitude
491.563 km
Semi-major axis
6,991.677 km
Eccentricity
0.01745
Inclination
97.6694°
RAAN
270.6053°
Arg. of periapsis
163.6311°
True anomaly
196.48927°
Mean anomaly
197.0639°
Eccentric anomaly
196.7754°
Mean motion
3.71254 °/min
Orbital period
96.97 mins
BSTAR
0.00019479
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Other satellites on launch #79 in the year 2019 (2019-11-25 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.OBJECT E 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 | 2025-09-18 13:05:24.475Z | 36.36° NE | 2025-09-18 13:08:24.475Z | 105.1° ESE | 28.146° | 2025-09-18 13:11:24.475Z | 162.523° S |
| 6 mins | 2025-09-18 23:59:24.475Z | 114.351° SE | 2025-09-19 00:01:24.475Z | 77.686° E | 25.72° | 2025-09-19 00:05:24.475Z | 12.032° NNE |
| 6 mins | 2025-09-19 01:35:24.475Z | 222.229° SW | 2025-09-19 01:37:24.475Z | 257.797° W | 24.188° | 2025-09-19 01:41:24.475Z | 321.208° 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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