SUNSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite SUNSAT at a glance.

Uptime

9569

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

96.5

Latest

Satellite identification and parameters

Extended collection of information and parameters for SUNSAT.

Object identification

Identified? True

Debris? False

Object name: SUNSAT

International designator: 1999-008C

Object number (NORAD): 25636

Object ID (CCSDS): 25636

Country: SOUTH AFRICA (SAFR)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 99.575 minutes

Inclination: 96.4654 deg

SMA: 7116.418 km

Apoapsis: 839.571 km

Periapsis: 636.995 km

RAAN: 93.1095 deg

Eccentricy: 0.014233

Argument of periapsis: 182.7187 deg

Mean anomaly: 177.3253 deg

Mean motion: 14.46140826 rev/day

Mean motion (dot): 0.0000032 rev/day2

B* drag term: 0.000086588 1/REarth

Two-line elements (TLE)

Creation date: May 6, 2025, 3:54 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 5, 2025, 8:07 p.m. UTC

TLE line 0: 0 SUNSAT

TLE line 1: 1 25636U 99008C 25125.83846697 .00000320 00000-0 86588-4 0 9998

TLE line 2: 2 25636 96.4654 93.1095 0142330 182.7187 177.3253 14.46140826380355

Live tracking on map

Real-time ground track for satellite SUNSAT.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
ARIANE 44L DEB (SPELDA) MEO 2025-04-29 21:17:29 0.0001899743 404.0 (m) DEBRIS
SL-8 R/B LEO 2025-04-29 15:52:59 0.0001949174 692.0 (m) ROCKET BODY
COSMOS 2251 DEB LEO 2025-04-11 08:45:28 0.0002438571 201.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-01-26 02:35:28 0.0001629425 97.0 (m) DEBRIS
IRIDIUM 33 DEB LEO 2024-12-22 05:17:56 0.0002673783 261.0 (m) DEBRIS

Associated space launch

ARGOS (Advanced Research & Global Observation Satellite) is a testbed and demonstration program for advanced remote sensing technologies for the US Air Force's Space Test Program (STP). ARGOS's primary objective is to fly and operate advanced payloads that include two technology demonstrations and seven experiment payloads for global and celestial observation. ARGOS also has a goal of three years of on orbit operations to demonstrate and collect science data for the Earth's global environment and top priority military space programs.

SUNSAT was lifted into orbit during the mission ‘Delta II | ARGOS’, on board a Delta II space rocket.

The launch took place on Feb. 23, 1999, 10:29 a.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | ARGOS
Delta II | ARGOS

Agency: N/A

Status: Launch Successful

Launch date: Feb. 23, 1999, 10:29 a.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

...

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