IRNSS-1I is a payload in GEO orbit, operated by Indian Space Research Organization, launched 2018.
| Orbit class | GEO |
| Inclination | 28.7973° |
| Eccentricity | 0.0018087 |
| Period | 1436.0 min |
| Apogee | 35,861 km |
| Perigee | 35,708 km |
| Mean motion | 1.00279237 rev/day |
| RAAN | 73.8917° |
| Arg of perigee | 180.4002° |
| Mean anomaly | 27.0525° |
| B* | 0.0000e+0 |
| Rev at epoch | 3,027 |
1 43286U 18035A 26187.83739036 .00000079 00000-0 00000-0 0 99992 43286 28.7973 73.8917 0018087 180.4002 27.0525 1.00279237 30279{
"OBJECT_NAME": "IRNSS-1I",
"OBJECT_ID": "2018-035A",
"EPOCH": "2026-07-06T20:05:50.527+00:00",
"MEAN_MOTION": 1.00279237,
"ECCENTRICITY": 0.0018087,
"INCLINATION": 28.7973,
"RA_OF_ASC_NODE": 73.8917,
"ARG_OF_PERICENTER": 180.4002,
"MEAN_ANOMALY": 27.0525,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 43286,
"REV_AT_EPOCH": 3027,
"BSTAR": 0,
"MEAN_MOTION_DOT": 7.9e-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 | IRNSS-1I |
| Operator | Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 1425HIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |