SKIPPER

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite SKIPPER at a glance.

Uptime

10782

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 SKIPPER.

Object identification

Identified? True

Debris? False

Object name: SKIPPER

International designator: 1995-072B

Object number (NORAD): 23752

Object ID (CCSDS): 23752

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.974 minutes

Inclination: 98.7792 deg

SMA: 7182.916 km

Apoapsis: 809.379 km

Periapsis: 800.183 km

RAAN: 252.0817 deg

Eccentricy: 0.0006401

Argument of periapsis: 62.0782 deg

Mean anomaly: 298.1045 deg

Mean motion: 14.26105315 rev/day

Mean motion (dot): -0.0000001 rev/day2

B* drag term: 0.000014446 1/REarth

Two-line elements (TLE)

Creation date: July 4, 2025, 6:39 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 4, 2025, 5:25 a.m. UTC

TLE line 0: 0 SKIPPER

TLE line 1: 1 23752U 95072B 25185.22598266 -.00000010 00000-0 14446-4 0 9998

TLE line 2: 2 23752 98.7792 252.0817 0006401 62.0782 298.1045 14.26105315535745

Live tracking on map

Real-time ground track for satellite SKIPPER.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SKIPPER.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-06-29 18:13:29 0.0001505188 865.0 (m) DEBRIS
CZ-2D DEB SSO 2025-01-27 07:27:35 0.0001773561 351.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-29 15:59:56 0.0001566274 502.0 (m) DEBRIS
THOR BURNER 2 R/B SSO 2024-11-25 12:24:57 0.0004711558 149.0 (m) ROCKET BODY
CZ-6A DEB LEO 2024-11-13 03:04:09 0.000119004 301.0 (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.

SKIPPER 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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