IRIDIUM 33 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite IRIDIUM 33 DEB at a glance.

Uptime

10100

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 33 DEB.

Object identification

Identified? True

Debris? True

Object name: IRIDIUM 33 DEB

International designator: 1997-051BF

Object number (NORAD): 33886

Object ID (CCSDS): 33886

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.295 minutes

Inclination: 86.3849 deg

SMA: 7150.664 km

Apoapsis: 781.273 km

Periapsis: 763.784 km

RAAN: 158.4391 deg

Eccentricy: 0.0012229

Argument of periapsis: 229.4894 deg

Mean anomaly: 180.7601 deg

Mean motion: 14.35764592 rev/day

Mean motion (dot): 0.00000555 rev/day2

B* drag term: 0.00018515 1/REarth

Two-line elements (TLE)

Creation date: May 10, 2025, 2:32 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 9, 2025, 10:31 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 33886U 97051BF 25129.93827014 .00000555 00000-0 18515-3 0 9991

TLE line 2: 2 33886 86.3849 158.4391 0012229 229.4894 180.7601 14.35764592849418

Live tracking on map

Real-time ground track for satellite IRIDIUM 33 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 33 DEB.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2024-12-26 01:47:34 0.0002890958 949.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-12 12:46:47 0.0001145069 933.0 (m) DEBRIS

Associated space launch

Iridium provides global mobile telecommunications services using a constellation of 66 low earth orbit satellites in a 86.4° inclined orbit. Although 77 satellites were originally envisioned for the system and spawned the name based on the 77th element in the periodic table, the system has been scaled back. Motorola's Satellite Communications Group designed and manufactured the Iridium satellites with Lockheed Martin providing the LM-700A spacecraft buses.

IRIDIUM 33 DEB was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 27 to 33’, on board a Proton-K/17S40 space rocket.

The launch took place on Sept. 14, 1997, 1:36 a.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 27 to 33
Proton-K/17S40 | Iridium 27 to 33

Agency: N/A

Status: Launch Successful

Launch date: Sept. 14, 1997, 1:36 a.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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