STEX

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite STEX at a glance.

Uptime

9934

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

85.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for STEX.

Object identification

Identified? True

Debris? False

Object name: STEX

International designator: 1998-055A

Object number (NORAD): 25489

Object ID (CCSDS): 25489

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 99.2 minutes

Inclination: 84.9829 deg

SMA: 7098.505 km

Apoapsis: 725.883 km

Periapsis: 714.858 km

RAAN: 86.9208 deg

Eccentricy: 0.00077659

Argument of periapsis: 328.9848 deg

Mean anomaly: 31.0896 deg

Mean motion: 14.5161812 rev/day

Mean motion (dot): 0.0000107 rev/day2

B* drag term: 0.00026188078 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, 6:05 a.m. UTC

TLE line 0: 0 STEX

TLE line 1: 1 25489U 98055A 25346.25349829 .00001070 00000-0 26188-3 0 9993

TLE line 2: 2 25489 84.9829 86.9208 0007766 328.9848 31.0896 14.51618120436213

Live tracking on map

Real-time ground track for satellite STEX.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
NOAA 17 DEB SSO 2025-12-12 09:01:03 0.0001831875 312.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-06-20 12:16:34 0.000668123 746.0 (m) DEBRIS
CZ-4 DEB SSO 2025-06-14 14:35:09 0.0003023308 440.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-30 15:17:17 0.0003653638 268.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-12 09:36:40 0.0001794229 163.0 (m) DEBRIS

Associated space launch

The STEX (Space Technology Experiments) satellite carried 29 new technologies intended to result in lower cost and higher performance spacecraft for future missions.

STEX was lifted into orbit during the mission ‘Minotaur | NROL-8’, on board a Minotaur space rocket.

The launch took place on Oct. 3, 1998, 10:04 a.m. from Space Launch Complex 576E.

For more information about the launch, click the button.

Launch to space Minotaur | NROL-8
Minotaur | NROL-8

Agency: N/A

Status: Launch Successful

Launch date: Oct. 3, 1998, 10:04 a.m. UTC

Rocket: Minotaur

Launch pad: Space Launch Complex 576E

Location: Vandenberg SFB, CA, USA

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