▸Orbital parameters

Orbit class	GEO
Inclination	0.0541°
Eccentricity	0.0003355
Period	1436.1 min
Apogee	35,801 km
Perigee	35,773 km
Mean motion	1.00270158 rev/day
RAAN	92.9269°
Arg of perigee	176.9352°
Mean anomaly	156.4053°
B*	0.0000e+0
Rev at epoch	2,039

▸Two-line element set (TLE)

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

1 47256U 20099A 26188.16152795 -.00000149 00000-0 00000-0 0 9990

2 47256 0.0541 92.9269 0003355 176.9352 156.4053 1.00270158 20394

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CMS-01",
  "OBJECT_ID": "2020-099A",
  "EPOCH": "2026-07-07T03:52:36.015+00:00",
  "MEAN_MOTION": 1.00270158,
  "ECCENTRICITY": 0.0003355,
  "INCLINATION": 0.0541,
  "RA_OF_ASC_NODE": 92.9269,
  "ARG_OF_PERICENTER": 176.9352,
  "MEAN_ANOMALY": 156.4053,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 47256,
  "REV_AT_EPOCH": 2039,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000149,
  "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-01
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	India
Launch date	Dec 17, 2020HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1410HIGHvia 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/47256

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