SCOT-1 (SCOT) is a payload in SSO orbit, operated by Digantara Research and Technologies / Orbital Astronautics, launched 2025.
| Orbit class | SSO |
| Inclination | 97.3849° |
| Eccentricity | 0.0004799 |
| Period | 92.5 min |
| Apogee | 400 km |
| Perigee | 394 km |
| Mean motion | 15.56790234 rev/day |
| RAAN | 276.1954° |
| Arg of perigee | 212.4965° |
| Mean anomaly | 147.5996° |
| B* | 8.6298e-4 |
| Rev at epoch | 8,238 |
1 62617U 25009J 26187.70248353 .00062097 00000-0 86298-3 0 99942 62617 97.3849 276.1954 0004799 212.4965 147.5996 15.56790234 82380{
"OBJECT_NAME": "SCOT-1 (SCOT)",
"OBJECT_ID": "2025-009J",
"EPOCH": "2026-07-06T16:51:34.577+00:00",
"MEAN_MOTION": 15.56790234,
"ECCENTRICITY": 0.0004799,
"INCLINATION": 97.3849,
"RA_OF_ASC_NODE": 276.1954,
"ARG_OF_PERICENTER": 212.4965,
"MEAN_ANOMALY": 147.5996,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 62617,
"REV_AT_EPOCH": 8238,
"BSTAR": 0.00086298,
"MEAN_MOTION_DOT": 0.00062097,
"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 | SCOT-1 (SCOT) |
| Operator | Digantara Research and Technologies / Orbital AstronauticsHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | India |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |