SKIPPER

Satellite information

Favourite Embed

Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite SKIPPER at a glance.

Uptime

10722

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: 100.975 minutes

Inclination: 98.7819 deg

SMA: 7182.941 km

Apoapsis: 808.161 km

Periapsis: 801.451 km

RAAN: 191.4647 deg

Eccentricy: 0.0004671

Argument of periapsis: 222.8215 deg

Mean anomaly: 137.2601 deg

Mean motion: 14.26097757 rev/day

Mean motion (dot): 0.00000045 rev/day2

B* drag term: 0.000037748 1/REarth

Two-line elements (TLE)

Creation date: May 5, 2025, 2:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 4, 2025, 5:56 p.m. UTC

TLE line 0: 0 SKIPPER

TLE line 1: 1 23752U 95072B 25124.74727357 .00000045 00000-0 37748-4 0 9990

TLE line 2: 2 23752 98.7819 191.4647 0004671 222.8215 137.2601 14.26097757527120

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
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
NOAA 16 DEB SSO 2024-09-05 23:08:32 0.0001775796 708.0 (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.