▸Orbital parameters

Orbit class	GEO
Inclination	0.0383°
Eccentricity	0.0001908
Period	1436.1 min
Apogee	35,794 km
Perigee	35,778 km
Mean motion	1.00272934 rev/day
RAAN	97.7736°
Arg of perigee	344.5838°
Mean anomaly	327.7974°
B*	0.0000e+0
Rev at epoch	609

▸Two-line element set (TLE)

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

1 62028U 24214A 26188.15849462 -.00000005 00000-0 00000-0 0 9991

2 62028 0.0383 97.7736 0001908 344.5838 327.7974 1.00272934 6098

▸ source OMM (JSON)

{
  "OBJECT_NAME": "GSAT-N2 (GSAT-20)",
  "OBJECT_ID": "2024-214A",
  "EPOCH": "2026-07-07T03:48:13.935+00:00",
  "MEAN_MOTION": 1.00272934,
  "ECCENTRICITY": 0.0001908,
  "INCLINATION": 0.0383,
  "RA_OF_ASC_NODE": 97.7736,
  "ARG_OF_PERICENTER": 344.5838,
  "MEAN_ANOMALY": 327.7974,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62028,
  "REV_AT_EPOCH": 609,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -5e-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	GSAT-N2 (GSAT-20)
Operator	New Space India LtdHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree NewSpace India LimitedMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Nov 18, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4700HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/62028

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