SL-3 R/B, 19046

Orbit data source: Space-Track

SL-3 R/B, 19046 is space debris in SSO originally from a launch on Wed, 20 Apr 1988 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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Identifier
19046, 1988-032B
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
Progress
Mission
Spacecraft
Bus & Motor
BLOK-E, Unknown motor
Mass
1,440 kg wet, 1,440 kg dry
Launch date (UTC)
1988-04-20 (38 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.9 m
Radar Cross Section
10.414 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 SL-3 R/B
1 19046U 88032B   26154.49148678  .00005014  00000-0  22948-3 0  9994
2 19046  97.5252 137.5478 0023817 296.5346  63.3448 15.20729526 65146
Epoch: 2026-06-03T11:47Z
TLE epoch observation values (Epoch: 2026-06-03T11:47:44.457Z)
Latitude
0.00001°
Longitude
68.66322°
Altitude
499.403 km
Speed
7.619 km/s
True Right ascension
09h 10m 11s
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
02:59:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.992 km
Perigee altitude
484.226 km
Semi-major axis
6,878.746 km
Eccentricity
0.00238
Inclination
97.5252°
RAAN
137.5478°
Arg. of periapsis
296.5346°
True anomaly
63.58904°
Mean anomaly
63.3448°
Eccentric anomaly
63.46689°
Mean motion
3.80434 °/min
Orbital period
94.63 mins
BSTAR
0.00022948
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Other satellites on launch #32 in the year 1988 (1988-04-20 UTC)

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