▸Orbital parameters

Orbit class	GEO
Inclination	0.0813°
Eccentricity	0.0001132
Period	1436.1 min
Apogee	35,791 km
Perigee	35,782 km
Mean motion	1.00272583 rev/day
RAAN	95.6917°
Arg of perigee	19.9367°
Mean anomaly	283.8998°
B*	0.0000e+0
Rev at epoch	4,726

▸Two-line element set (TLE)

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

1 58990U 24033A 26188.08999720 -.00000141 00000-0 00000-0 0 9999

2 58990 0.0813 95.6917 0001132 19.9367 283.8998 1.00272583 47268

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INSAT-3DS",
  "OBJECT_ID": "2024-033A",
  "EPOCH": "2026-07-07T02:09:35.758+00:00",
  "MEAN_MOTION": 1.00272583,
  "ECCENTRICITY": 0.0001132,
  "INCLINATION": 0.0813,
  "RA_OF_ASC_NODE": 95.6917,
  "ARG_OF_PERICENTER": 19.9367,
  "MEAN_ANOMALY": 283.8998,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58990,
  "REV_AT_EPOCH": 4726,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000141,
  "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	INSAT-3DS
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	India
Launch date	Feb 17, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	2275HIGHvia 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/58990

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