SKIPPER

Satellite information

Favourite Embed

Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite SKIPPER at a glance.

Uptime

10943

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: 100.972 minutes

Inclination: 98.76 deg

SMA: 7182.826 km

Apoapsis: 808.042 km

Periapsis: 801.34 km

RAAN: 53.1864 deg

Eccentricy: 0.0004665

Argument of periapsis: 316.7849 deg

Mean anomaly: 43.2964 deg

Mean motion: 14.26132136 rev/day

Mean motion (dot): 0.00000056 rev/day2

B* drag term: 0.000042282421 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 4:09 a.m. UTC

TLE line 0: 0 SKIPPER

TLE line 1: 1 23752U 95072B 25346.17341048 .00000056 00000-0 42282-4 0 9993

TLE line 2: 2 23752 98.7600 53.1864 0004665 316.7849 43.2964 14.26132136558686

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

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.