SL-6 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-6 R/B at a glance.

Uptime

10784

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-6 R/B.

Object identification

Identified? True

Debris? False

Object name: SL-6 R/B

International designator: 1995-072C

Object number (NORAD): 23753

Object ID (CCSDS): 23753

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.915 minutes

Inclination: 98.7498 deg

SMA: 7180.085 km

Apoapsis: 804.906 km

Periapsis: 798.995 km

RAAN: 254.1103 deg

Eccentricy: 0.0004116

Argument of periapsis: 33.2079 deg

Mean anomaly: 326.9358 deg

Mean motion: 14.26948665 rev/day

Mean motion (dot): 0.00000034 rev/day2

B* drag term: 0.000032394 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 3:08 p.m. UTC

TLE line 0: 0 SL-6 R/B

TLE line 1: 1 23753U 95072C 25187.63076333 .00000034 00000-0 32394-4 0 9999

TLE line 2: 2 23753 98.7498 254.1103 0004116 33.2079 326.9358 14.26948665536639

Live tracking on map

Real-time ground track for satellite SL-6 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-6 R/B.

Target Orbit TCA Probability of collision Miss distance Type
THOR ABLESTAR DEB LEO 2025-06-10 14:09:25 0.0001173755 348.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-05-18 14:48:42 0.0001347193 352.0 (m) DEBRIS
CZ-4 DEB SSO 2025-03-24 17:32:36 0.0001494398 553.0 (m) DEBRIS
THOR ABLESTAR DEB LEO 2025-01-19 14:02:35 0.0001107073 436.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-01-12 04:57:40 0.0001015815 443.0 (m) DEBRIS

Associated space launch

IRS 1C and 1D (Indian Remote Sensing Satellite) were the second version of the series of indigenous state-of-art remote sensing satellites. Skipper was an international project initiated by BMDO to measure the bow-shock UV emissions from reentering bodies at different speeds and heights.

SL-6 R/B was lifted into orbit during the mission ‘Molniya-M | IRS-1C & Skipper’, on board a Molniya-M space rocket.

The launch took place on Dec. 28, 1995, 6:45 a.m. from 31/6.

For more information about the launch, click the button.

Launch to space Molniya-M | IRS-1C & Skipper
Molniya-M | IRS-1C & Skipper

Agency: N/A

Status: Launch Successful

Launch date: Dec. 28, 1995, 6:45 a.m. UTC

Rocket: Molniya-M

Launch pad: 31/6

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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