▸Orbital parameters

Orbit class	GEO
Inclination	0.0449°
Eccentricity	0.0000369
Period	1436.2 min
Apogee	35,790 km
Perigee	35,787 km
Mean motion	1.00264910 rev/day
RAAN	259.9546°
Arg of perigee	6.4894°
Mean anomaly	69.8299°
B*	0.0000e+0
Rev at epoch	8,075

▸Two-line element set (TLE)

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

1 28358U 04022A 26188.14488786 .00000003 00000-0 00000-0 0 9998

2 28358 0.0449 259.9546 0000369 6.4894 69.8299 1.00264910 80750

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 10-02",
  "OBJECT_ID": "2004-022A",
  "EPOCH": "2026-07-07T03:28:38.311+00:00",
  "MEAN_MOTION": 1.0026491,
  "ECCENTRICITY": 0.0000369,
  "INCLINATION": 0.0449,
  "RA_OF_ASC_NODE": 259.9546,
  "ARG_OF_PERICENTER": 6.4894,
  "MEAN_ANOMALY": 69.8299,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 28358,
  "REV_AT_EPOCH": 8075,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 3e-8,
  "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	INTELSAT 10-02
Operator	Intelsat Ltd, US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jun 16, 2004HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5575HIGHvia 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/28358

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