INSAT-3DR is a payload in GEO orbit, operated by Indian Space Research Organization, launched 2016.
| Orbit class | GEO |
| Inclination | 0.0487° |
| Eccentricity | 0.0010406 |
| Period | 1436.1 min |
| Apogee | 35,830 km |
| Perigee | 35,743 km |
| Mean motion | 1.00272313 rev/day |
| RAAN | 89.5096° |
| Arg of perigee | 181.2031° |
| Mean anomaly | 120.1823° |
| B* | 0.0000e+0 |
| Rev at epoch | 3,601 |
1 41752U 16054A 26188.08843720 -.00000062 00000-0 00000-0 0 99912 41752 0.0487 89.5096 0010406 181.2031 120.1823 1.00272313 36010{
"OBJECT_NAME": "INSAT-3DR",
"OBJECT_ID": "2016-054A",
"EPOCH": "2026-07-07T02:07:20.974+00:00",
"MEAN_MOTION": 1.00272313,
"ECCENTRICITY": 0.0010406,
"INCLINATION": 0.0487,
"RA_OF_ASC_NODE": 89.5096,
"ARG_OF_PERICENTER": 181.2031,
"MEAN_ANOMALY": 120.1823,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 41752,
"REV_AT_EPOCH": 3601,
"BSTAR": 0,
"MEAN_MOTION_DOT": -6.2e-7,
"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.
| Name | INSAT-3DR |
| Operator | Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 2211HIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |