▸Orbital parameters

Orbit class	LEO
Inclination	86.4219°
Eccentricity	0.0001693
Period	100.1 min
Apogee	764 km
Perigee	762 km
Mean motion	14.38612974 rev/day
RAAN	16.9051°
Arg of perigee	95.1525°
Mean anomaly	264.9867°
B*	7.0386e-5
Rev at epoch	39,307

▸Two-line element set (TLE)

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

1 43926U 19002E 26188.00606588 .00000235 00000-0 70386-4 0 9992

2 43926 86.4219 16.9051 0001693 95.1525 264.9867 14.38612974393073

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDIUM 169",
  "OBJECT_ID": "2019-002E",
  "EPOCH": "2026-07-07T00:08:44.092+00:00",
  "MEAN_MOTION": 14.38612974,
  "ECCENTRICITY": 0.0001693,
  "INCLINATION": 86.4219,
  "RA_OF_ASC_NODE": 16.9051,
  "ARG_OF_PERICENTER": 95.1525,
  "MEAN_ANOMALY": 264.9867,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43926,
  "REV_AT_EPOCH": 39307,
  "BSTAR": 0.000070386,
  "MEAN_MOTION_DOT": 0.00000235,
  "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 169
Operator	Iridium Satellite LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 11, 2019HIGHvia 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/43926

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