▸Orbital parameters

Orbit class	LEO
Inclination	86.3951°
Eccentricity	0.0002281
Period	100.4 min
Apogee	779 km
Perigee	776 km
Mean motion	14.34217759 rev/day
RAAN	80.2384°
Arg of perigee	85.0865°
Mean anomaly	275.0591°
B*	-1.2444e-6
Rev at epoch	49,609

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 41920U 17003D 26187.80192382 .00000016 00000-0 -12444-5 0 9992

2 41920 86.3951 80.2384 0002281 85.0865 275.0591 14.34217759496090

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDIUM 102",
  "OBJECT_ID": "2017-003D",
  "EPOCH": "2026-07-06T19:14:46.218+00:00",
  "MEAN_MOTION": 14.34217759,
  "ECCENTRICITY": 0.0002281,
  "INCLINATION": 86.3951,
  "RA_OF_ASC_NODE": 80.2384,
  "ARG_OF_PERICENTER": 85.0865,
  "MEAN_ANOMALY": 275.0591,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41920,
  "REV_AT_EPOCH": 49609,
  "BSTAR": -0.0000012444,
  "MEAN_MOTION_DOT": 1.6e-7,
  "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 102
Operator	Iridium Satellite LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 14, 2017HIGHvia 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/41920

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