STEX

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite STEX at a glance.

Uptime

9882

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: 99.207 minutes

Inclination: 84.9792 deg

SMA: 7098.848 km

Apoapsis: 728.253 km

Periapsis: 713.172 km

RAAN: 117.0301 deg

Eccentricy: 0.00106225

Argument of periapsis: 118.6697 deg

Mean anomaly: 241.5575 deg

Mean motion: 14.51513171 rev/day

Mean motion (dot): 0.00000982 rev/day2

B* drag term: 0.00024036573 1/REarth

Two-line elements (TLE)

Creation date: Oct. 23, 2025, 2:46 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 22, 2025, 10:21 p.m. UTC

TLE line 0: 0 STEX

TLE line 1: 1 25489U 98055A 25295.93127713 .00000982 00000-0 24037-3 0 9999

TLE line 2: 2 25489 84.9792 117.0301 0010622 118.6697 241.5575 14.51513171428913

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 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
THORAD AGENA D DEB LEO 2024-10-16 15:11:04 0.000292892 885.0 (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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