▸Orbital parameters

Orbit class	LEO
Inclination	86.3946°
Eccentricity	0.0002182
Period	100.4 min
Apogee	779 km
Perigee	776 km
Mean motion	14.34217994 rev/day
RAAN	79.9954°
Arg of perigee	81.9953°
Mean anomaly	278.1490°
B*	6.8497e-5
Rev at epoch	42,534

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 43479U 18047D 26188.12540506 .00000212 00000-0 68497-4 0 9998

2 43479 86.3946 79.9954 0002182 81.9953 278.1490 14.34217994425349

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDIUM 152",
  "OBJECT_ID": "2018-047D",
  "EPOCH": "2026-07-07T03:00:34.997+00:00",
  "MEAN_MOTION": 14.34217994,
  "ECCENTRICITY": 0.0002182,
  "INCLINATION": 86.3946,
  "RA_OF_ASC_NODE": 79.9954,
  "ARG_OF_PERICENTER": 81.9953,
  "MEAN_ANOMALY": 278.149,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43479,
  "REV_AT_EPOCH": 42534,
  "BSTAR": 0.000068497,
  "MEAN_MOTION_DOT": 0.00000212,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	IRIDIUM 152
Operator	Iridium Satellite LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	May 22, 2018HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	860HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/43479

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.