DUMMY SAT 2/BREEZE-M, 40355
Orbit data source: Space-Track
DUMMY SAT 2/BREEZE-M, 40355 is a payload satellite owned by Khrunichev (CIS) in GEO that was launched on Tue, 23 Dec 2014 UTC via an ANGARA A5 launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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40355 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Khrunichev
Mission
Non-operational Civil Technology
Bus & Motor
GVM, Unknown motor
Mass
~3,600 kg wet, 2,042 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Flared Cyl, 2.0 m
Radar Cross Section
7.854 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 DUMMY SAT 2/BREEZE-M
1 40355U 14085A 26070.06317101 -.00000130 00000-0 00000+0 0 9993
2 40355 10.0708 61.5312 0368465 351.8243 7.6477 0.94060296 38290Epoch: 2026-03-11T01:30Z
TLE epoch observation values (Epoch: 2026-03-11T01:30:57.975Z)
Latitude
0.00001°
Longitude
-129.85914°
Altitude
36,021.798 km
Speed
3.121 km/s
True Right ascension
04h 06m 27s
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
13:18:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,245.348 km
Perigee altitude
36,002.697 km
Semi-major axis
44,002.16 km
Eccentricity
0.03685
Inclination
10.0708°
RAAN
61.5312°
Arg. of periapsis
351.8243°
True anomaly
8.23642°
Mean anomaly
7.6477°
Eccentric anomaly
7.9393°
Mean motion
0.23514 °/min
Orbital period
1,530.98 mins
BSTAR
0
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Other satellites on launch #85 in the year 2014 (2014-12-23 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.DUMMY SAT 2/BREEZE-M 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. |
|---|---|---|---|---|---|---|---|
| 477 mins | 2026-03-12 08:58:24.913Z | 250.585° W | 2026-03-12 08:58:24.913Z | 250.585° W | 25.919° | 2026-03-12 16:55:24.913Z | 250.724° W |
| 23 mins | 2026-03-13 08:35:24.913Z | 265.952° W | 2026-03-13 08:58:24.913Z | 266.425° W | 10.187° | 2026-03-13 08:58:24.913Z | 266.425° W |
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40355 neighbors
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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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