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

10214

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.0

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: 1997-051AAJ

Object number (NORAD): 39777

Object ID (CCSDS): 39777

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.054 minutes

Inclination: 85.9593 deg

SMA: 7091.544 km

Apoapsis: 757.172 km

Periapsis: 669.646 km

RAAN: 227.0033 deg

Eccentricy: 0.00617115

Argument of periapsis: 185.9894 deg

Mean anomaly: 174.0583 deg

Mean motion: 14.53756031 rev/day

Mean motion (dot): 0.00005953 rev/day2

B* drag term: 0.0013793796 1/REarth

Two-line elements (TLE)

Creation date: Aug. 27, 2025, 8:01 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 27, 2025, 9:17 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 39777U 97051AAJ 25239.38704412 .00005953 00000-0 13794-2 0 9993

TLE line 2: 2 39777 85.9593 227.0033 0061712 185.9894 174.0583 14.53756031586240

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
START 1 DEB LEO 2025-06-30 18:39:51 0.0001770709 42.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-17 02:24:31 0.0002738604 858.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-14 06:53:50 0.0001236459 754.0 (m) DEBRIS
JAWSAT SSO 2024-11-03 06:06:51 0.0001077386 438.0 (m) PAYLOAD

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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