GMS-T is a payload in LEO orbit, operated by OHB (Orbital Hochtechnologie Bremen System GmbH) / Shanghai Spacecom Satellite Technology Ltd, launched 2021.
| Orbit class | LEO |
| Inclination | 90.1283° |
| Eccentricity | 0.0002837 |
| Period | 109.4 min |
| Apogee | 1,200 km |
| Perigee | 1,195 km |
| Mean motion | 13.16657112 rev/day |
| RAAN | 242.0755° |
| Arg of perigee | 32.0791° |
| Mean anomaly | 328.0513° |
| B* | -8.8546e-6 |
| Rev at epoch | 26,221 |
1 47346U 21004A 26188.07384455 .00000005 00000-0 -88546-5 0 99942 47346 90.1283 242.0755 0002837 32.0791 328.0513 13.16657112262214{
"OBJECT_NAME": "GMS-T",
"OBJECT_ID": "2021-004A",
"EPOCH": "2026-07-07T01:46:20.169+00:00",
"MEAN_MOTION": 13.16657112,
"ECCENTRICITY": 0.0002837,
"INCLINATION": 90.1283,
"RA_OF_ASC_NODE": 242.0755,
"ARG_OF_PERICENTER": 32.0791,
"MEAN_ANOMALY": 328.0513,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 47346,
"REV_AT_EPOCH": 26221,
"BSTAR": -0.0000088546,
"MEAN_MOTION_DOT": 5e-8,
"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 | GMS-T |
| Operator | OHB (Orbital Hochtechnologie Bremen System GmbH) / Shanghai Spacecom Satellite Technology LtdHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | Germany |
| Launch date | |
| Launch mass (kg) |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |