TJS-17 is a payload in GEO orbit, operated by Strategic Support Troops, launched 2025.
Orbital data last updated 4 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | GEO |
| Inclination | 1.1020° |
| Eccentricity | 0.0001564 |
| Period | 1436.1 min |
| Apogee | 35,793 km |
| Perigee | 35,780 km |
| Mean motion | 1.00271016 rev/day |
| RAAN | 82.5843° |
| Arg of perigee | 315.8143° |
| Mean anomaly | 326.1705° |
| B* | 0.0000e+0 |
| Rev at epoch | 444 |
1 63524U 25073A 26183.77560742 -.00000059 00000-0 00000-0 0 99902 63524 1.1020 82.5843 0001564 315.8143 326.1705 1.00271016 4441{
"OBJECT_NAME": "TJS-17",
"OBJECT_ID": "2025-073A",
"EPOCH": "2026-07-02T18:36:52.481+00:00",
"MEAN_MOTION": 1.00271016,
"ECCENTRICITY": 0.0001564,
"INCLINATION": 1.102,
"RA_OF_ASC_NODE": 82.5843,
"ARG_OF_PERICENTER": 315.8143,
"MEAN_ANOMALY": 326.1705,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 63524,
"REV_AT_EPOCH": 444,
"BSTAR": 0,
"MEAN_MOTION_DOT": -5.9e-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 | TJS-17 |
| Operator | |
| Country | China |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |