SL-16 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-16 R/B at a glance.

Uptime

10001

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

LEO

Low Earth Orbit

Inclination

71.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-16 R/B.

Object identification

Identified? True

Debris? False

Object name: SL-16 R/B

International designator: 1998-045B

Object number (NORAD): 25407

Object ID (CCSDS): 25407

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.682 minutes

Inclination: 71.0117 deg

SMA: 7216.455 km

Apoapsis: 843.294 km

Periapsis: 833.346 km

RAAN: 2.8891 deg

Eccentricy: 0.00068925

Argument of periapsis: 176.3806 deg

Mean anomaly: 183.7369 deg

Mean motion: 14.16174963 rev/day

Mean motion (dot): -0.00000158 rev/day2

B* drag term: -0.000055909078 1/REarth

Two-line elements (TLE)

Creation date: Dec. 14, 2025, 3:07 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 13, 2025, 11:18 a.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 25407U 98045B 25347.47104697 -.00000158 00000-0 -55909-4 0 9991

TLE line 2: 2 25407 71.0117 2.8891 0006893 176.3806 183.7369 14.16174963414897

Live tracking on map

Real-time ground track for satellite SL-16 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-16 R/B.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-10-10 16:11:52 0.0001049248 825.0 (m) DEBRIS
CZ-6A DEB SSO 2025-10-05 09:48:18 0.00396532 61.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-10-05 04:57:43 0.0001394033 705.0 (m) DEBRIS
CZ-6A DEB LEO 2025-05-06 01:48:44 0.001206164 70.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-27 19:29:09 0.0004874052 156.0 (m) DEBRIS

Associated space launch

Second generation ELING satellite

SL-16 R/B was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 20’, on board a Zenit-2 space rocket.

The launch took place on July 28, 1998, 9:15 a.m. from 45/1.

For more information about the launch, click the button.

Launch to space Zenit-2 | Tselina-2 20
Zenit-2 | Tselina-2 20

Agency: N/A

Status: Launch Successful

Launch date: July 28, 1998, 9:15 a.m. UTC

Rocket: Zenit-2

Launch pad: 45/1

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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