FREGAT R/B, 41106

Orbit data source: Space-Track

FREGAT R/B, 41106 is space debris in GEO originally from a launch on Fri, 11 Dec 2015 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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https://www.satcat.com/sats-embedded/41106?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41106, 2015-074B

Orbit

GEO

Last TLE update

1 day ago

Origin

Federal Space Agency of Russia (Roscosmos) (CIS)

Manufacturer

Lavochkin

Mission

Spacecraft

Bus & Motor

FREGAT, Unknown motor

Mass

1,000 kg wet, 1,000 kg dry

Launch date (UTC)

2015-12-11 (10 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 3.3 m

Radar Cross Section

8.683 m²

Expand to show TLE details & history

TLE from 1 day ago

0 FREGAT R/B
1 41106U 15074B   25182.68495512 -.00000275  00000-0  00000-0 0  9992
2 41106   7.2987  65.8955 0197530 349.4151  10.1164  1.02895901 35902

Epoch: 2025-07-01T16:26Z

TLE epoch observation values (Epoch: 2025-07-01T16:26:20.122Z)

Latitude

-0°

Longitude

-100.72266°

Altitude

34,260.317 km

Speed

3.162 km/s

True Right ascension

04h 23m 21s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

6.93691°

Longitude

-29.51867°

Altitude

34,930.807 km

Speed

3.111 km/s

Apparent Right ascension

09h 17m 13s

Apparent Declination

1° 26' 20"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

08:00:00

Azimuth

150.584° SSE

Elevation

47.71°

Doppler factor

Orbital elements

Apogee altitude

35,886.381 km

Perigee altitude

34,249.022 km

Semi-major axis

41,445.838 km

Eccentricity

0.01975

Inclination

7.2987°

RAAN

65.8955°

Arg. of periapsis

349.4151°

True anomaly

Unknown

Mean anomaly

10.1164°

Eccentric anomaly

Unknown

Mean motion

0.25723 °/min

Orbital period

1,399.53 mins

BSTAR

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41106 neighbors

Authenticating...

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Other satellites on launch #74 in the year 2015 (2015-12-11 UTC)

ELEKTRO-L 2, 41105

SL-23 R/B, 41107 (Decayed)

FREGAT DEB (TANK), 41108

SL-23 DEB, 41109 (Decayed)

SL-23 DEB, 41110 (Decayed)

SL-23 DEB, 41111 (Decayed)

SL-23 DEB, 41112 (Decayed)

FREGAT DEB, 41113 (Decayed)

FREGAT DEB, 41114 (Decayed)

FREGAT DEB, 41115 (Decayed)

FREGAT R/B Visibility forecast

Observer location: undefined°, undefined°

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.
1440 mins	2025-07-02 20:15:59.774Z	150.596° SSE	2025-07-02 21:14:59.774Z	149.551° SSE	36.572°	2025-07-03 20:15:59.774Z	136.763° SSE

Authenticating...

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Check out FREGAT R/B, 41106 on other resources

View FREGAT R/B, 41106 on Heavens-Above

View FREGAT R/B, 41106 on Keep Track

View FREGAT R/B, 41106 on Celestrak

View FREGAT R/B, 41106 on Gunter's Space Page

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