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

10723

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.8

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: 100.916 minutes

Inclination: 98.7525 deg

SMA: 7180.127 km

Apoapsis: 804.63 km

Periapsis: 799.354 km

RAAN: 193.2262 deg

Eccentricy: 0.0003674

Argument of periapsis: 176.7756 deg

Mean anomaly: 183.3448 deg

Mean motion: 14.269362 rev/day

Mean motion (dot): 0.00000063 rev/day2

B* drag term: 0.000044492 1/REarth

Two-line elements (TLE)

Creation date: May 7, 2025, 3:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 6, 2025, 6:24 p.m. UTC

TLE line 0: 0 SL-6 R/B

TLE line 1: 1 23753U 95072C 25126.76694596 .00000063 00000-0 44492-4 0 9997

TLE line 2: 2 23753 98.7525 193.2262 0003674 176.7756 183.3448 14.26936200527954

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
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
METEOR 2-5 DEB LEO 2024-08-08 21:28:00 0.001371405 47.0 (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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