▸Orbital parameters

Orbit class	GEO
Inclination	1.8534°
Eccentricity	0.0003753
Period	1436.1 min
Apogee	35,803 km
Perigee	35,771 km
Mean motion	1.00270512 rev/day
RAAN	82.3902°
Arg of perigee	27.7420°
Mean anomaly	38.7679°
B*	0.0000e+0
Rev at epoch	5,348

▸Two-line element set (TLE)

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

1 37392U 11016A 26187.71099740 -.00000211 00000-0 00000-0 0 9999

2 37392 1.8534 82.3902 0003753 27.7420 38.7679 1.00270512 53489

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 28 (IS-28)",
  "OBJECT_ID": "2011-016A",
  "EPOCH": "2026-07-06T17:03:50.175+00:00",
  "MEAN_MOTION": 1.00270512,
  "ECCENTRICITY": 0.0003753,
  "INCLINATION": 1.8534,
  "RA_OF_ASC_NODE": 82.3902,
  "ARG_OF_PERICENTER": 27.742,
  "MEAN_ANOMALY": 38.7679,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 37392,
  "REV_AT_EPOCH": 5348,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000211,
  "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 28 (IS-28)
Operator	New Dawn Satellite Co. (Intelsat/Convergence Partners)HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	MU
Launch date	Apr 22, 2011HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3000HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/37392

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