▸Orbital parameters

Orbit class	GEO
Inclination	0.0131°
Eccentricity	0.0000864
Period	1436.1 min
Apogee	35,791 km
Perigee	35,784 km
Mean motion	1.00268669 rev/day
RAAN	50.4978°
Arg of perigee	305.3940°
Mean anomaly	44.6143°
B*	0.0000e+0
Rev at epoch	1,480

▸Two-line element set (TLE)

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

1 52903U 22067A 26188.09017056 .00000000 00000-0 00000-0 0 9999

2 52903 0.0131 50.4978 0000864 305.3940 44.6143 1.00268669 14804

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CMS-02 (GSAT-24)",
  "OBJECT_ID": "2022-067A",
  "EPOCH": "2026-07-07T02:09:50.736+00:00",
  "MEAN_MOTION": 1.00268669,
  "ECCENTRICITY": 0.0000864,
  "INCLINATION": 0.0131,
  "RA_OF_ASC_NODE": 50.4978,
  "ARG_OF_PERICENTER": 305.394,
  "MEAN_ANOMALY": 44.6143,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 52903,
  "REV_AT_EPOCH": 1480,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0,
  "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	CMS-02 (GSAT-24)
Operator	New Space India LtdHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree NewSpace India LimitedMEDIUMvia Wikidata
Country	India
Launch date	Jun 22, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4181HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/52903

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