Showing default

LUCH 1, 23680

Orbit data source: Space-Track

LUCH 1, 23680 is a payload satellite owned by VKS (CIS) in GEO that was launched on Wed, 11 Oct 1995 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.

Not visible in the next 10 days
Identifier
23680, 1995-054A
Orbit
GEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO PM
Mission
Defense Communications
Bus & Motor
KAUR-4 AL'TAIR, Unknown motor
Mass
2,400 kg wet, ~2,200 kg dry
Launch date (UTC)
1995-10-11 (31 years ago)
Launch vehicle
PROTON-K/DM-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Pan + 2 Dish, 8.0 m
Radar Cross Section
40.926 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 LUCH 1
1 23680U 95054A   26207.61201205 -.00000091  00000-0  00000-0 0  9997
2 23680  15.0399 358.9242 0006714 148.8859  89.9897  1.00268984112745
Epoch: 2026-07-26T14:41Z
TLE epoch observation values (Epoch: 2026-07-26T14:41:17.841Z)
Latitude
-12.8586°
Longitude
72.35448°
Altitude
35,789.78 km
Speed
3.075 km/s
True Right ascension
15h 47m 56s
True Declination
-12° 50' 46"
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
23:13:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,816.656 km
Perigee altitude
35,760.034 km
Semi-major axis
42,166.482 km
Eccentricity
0.00067
Inclination
15.0399°
RAAN
358.9242°
Arg. of periapsis
148.8859°
True anomaly
90.06664°
Mean anomaly
89.9897°
Eccentric anomaly
90.02817°
Mean motion
0.25066 °/min
Orbital period
1,436.18 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|