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

10096

Days in orbit

Revolutions

≈ 14.5

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: 1997-051BA

Object number (NORAD): 33881

Object ID (CCSDS): 33881

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.128 minutes

Inclination: 86.3927 deg

SMA: 7095.107 km

Apoapsis: 761.937 km

Periapsis: 672.007 km

RAAN: 202.2522 deg

Eccentricy: 0.0063375

Argument of periapsis: 187.5126 deg

Mean anomaly: 349.0787 deg

Mean motion: 14.5266116 rev/day

Mean motion (dot): 0.00020776 rev/day2

B* drag term: 0.0049258 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, 10:57 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 33881U 97051BA 25125.95651150 .00020776 00000-0 49258-2 0 9994

TLE line 2: 2 33881 86.3927 202.2522 0063375 187.5126 349.0787 14.52661160842902

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
SAC C SSO 2025-04-02 09:47:31 0.0001149647 482.0 (m) PAYLOAD
CZ-6A DEB SSO 2025-02-10 13:11:14 0.001282699 39.0 (m) DEBRIS
METEOR 2-5 DEB LEO 2024-11-15 01:48:46 0.0004479281 574.0 (m) DEBRIS
CBERS 2 SSO 2024-06-26 12:50:04 0.0003141559 470.0 (m) PAYLOAD
NOAA 12 DEB SSO 2024-06-12 11:02:58 0.0003114421 60.0 (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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