DONGPO 10 is a payload in SSO orbit, operated by Chang Guang Satellite Technology Ltd / Meishan Huantian Smart Tech Co Ltd, launched 2022.
| Orbit class | SSO |
| Inclination | 97.6964° |
| Eccentricity | 0.0005625 |
| Period | 93.8 min |
| Apogee | 465 km |
| Perigee | 457 km |
| Mean motion | 15.34886405 rev/day |
| RAAN | 359.2095° |
| Arg of perigee | 52.8460° |
| Mean anomaly | 307.3296° |
| B* | 2.4559e-4 |
| Rev at epoch | 19,843 |
1 54689U 22167H 26188.21909411 .00008227 00000-0 24559-3 0 99992 54689 97.6964 359.2095 0005625 52.8460 307.3296 15.34886405198430{
"OBJECT_NAME": "DONGPO 10",
"OBJECT_ID": "2022-167H",
"EPOCH": "2026-07-07T05:15:29.731+00:00",
"MEAN_MOTION": 15.34886405,
"ECCENTRICITY": 0.0005625,
"INCLINATION": 97.6964,
"RA_OF_ASC_NODE": 359.2095,
"ARG_OF_PERICENTER": 52.846,
"MEAN_ANOMALY": 307.3296,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 54689,
"REV_AT_EPOCH": 19843,
"BSTAR": 0.00024559,
"MEAN_MOTION_DOT": 0.00008227,
"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 | DONGPO 10 |
| Operator | Chang Guang Satellite Technology Ltd / Meishan Huantian Smart Tech Co LtdHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | China |
| 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 |