NVS-02 (IRNSS-1K) is a payload in HEO orbit, operated by Indian Space Research Organization, launched 2025.
Orbital data last updated 46 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | HEO |
| Inclination | 20.7487° |
| Eccentricity | 0.7347988 |
| Period | 660.7 min |
| Apogee | 37,216 km |
| Perigee | 286 km |
| Mean motion | 2.17939568 rev/day |
| RAAN | 268.6914° |
| Arg of perigee | 132.0494° |
| Mean anomaly | 319.2185° |
| B* | 4.4019e-4 |
| Rev at epoch | 1,041 |
1 62850U 25020A 26142.16237527 .00000388 00000-0 44019-3 0 99982 62850 20.7487 268.6914 7347988 132.0494 319.2185 2.17939568 10411{
"OBJECT_NAME": "NVS-02 (IRNSS-1K)",
"OBJECT_ID": "2025-020A",
"EPOCH": "2026-05-22T03:53:49.223+00:00",
"MEAN_MOTION": 2.17939568,
"ECCENTRICITY": 0.7347988,
"INCLINATION": 20.7487,
"RA_OF_ASC_NODE": 268.6914,
"ARG_OF_PERICENTER": 132.0494,
"MEAN_ANOMALY": 319.2185,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 62850,
"REV_AT_EPOCH": 1041,
"BSTAR": 0.00044019,
"MEAN_MOTION_DOT": 0.00000388,
"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 | NVS-02 (IRNSS-1K) |
| Operator | Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 2232HIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |