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

Country

CIS

Related business

Federal Space Agency of Russia (Roscosmos) (RU)

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, 1.6 m

Radar Cross Section

8.683 m²

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Last TLE update: 22 hours ago

TLE from 22 hours ago

0 FREGAT R/B
1 41106U 15074B   26002.33145040 -.00000056  00000-0  00000-0 0  9991
2 41106   7.7357  63.7774 0196939 354.1485   5.5442  1.02893632 37806

Epoch: 2026-01-02T07:57Z

TLE epoch observation values (Epoch: 2026-01-02T07:57:17.314Z)

Latitude

0.00001°

Longitude

-157.60137°

Altitude

34,253.646 km

Speed

3.163 km/s

True Right ascension

04h 14m 46s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

05:43:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,884.55 km

Perigee altitude

34,252.065 km

Semi-major axis

41,446.445 km

Eccentricity

0.01969

Inclination

7.7357°

RAAN

63.7774°

Arg. of periapsis

354.1485°

True anomaly

5.7677°

Mean anomaly

5.5442°

Eccentric anomaly

5.6554°

Mean motion

0.25722 °/min

Orbital period

1,399.56 mins

BSTAR

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

SL-23 R/B, 41107 (Decayed)

ELEKTRO-L 2, 41105

SL-23 DEB, 41109 (Decayed)

SL-23 DEB, 41110 (Decayed)

SL-23 DEB, 41111 (Decayed)

FREGAT DEB (TANK), 41108

FREGAT DEB, 41113 (Decayed)

SL-23 DEB, 41112 (Decayed)

FREGAT DEB, 41115 (Decayed)

FREGAT DEB, 41114 (Decayed)

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FREGAT R/B 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.
1440 mins	2026-01-03 05:52:18.536Z	234.684° WSW	2026-01-03 13:39:18.536Z	237.572° WSW	30.18°	2026-01-04 05:52:18.536Z	226.141° WSW

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41106 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

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out FREGAT R/B, 41106 on other resources

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View FREGAT R/B, 41106 on Celestrak

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

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FREGAT R/B, 41106

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 22 hours ago

TLE from 22 hours ago

TLE epoch observation values (Epoch: 2026-01-02T07:57:17.314Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

FREGAT R/B Visibility forecast

41106 neighbors

Co-orbital & Co-planar RSOs

Check out FREGAT R/B, 41106 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 22 hours ago