DONGPO 09 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 | 97.6918° |
| Eccentricity | 0.0003261 |
| Period | 93.7 min |
| Apogee | 458 km |
| Perigee | 453 km |
| Mean motion | 15.36806567 rev/day |
| RAAN | 0.1156° |
| Arg of perigee | 70.4343° |
| Mean anomaly | 289.7252° |
| B* | 2.5289e-4 |
| Rev at epoch | 19,852 |
1 54685U 22167D 26188.20721160 .00009011 00000-0 25289-3 0 99902 54685 97.6918 0.1156 0003261 70.4343 289.7252 15.36806567198523{
"OBJECT_NAME": "DONGPO 09",
"OBJECT_ID": "2022-167D",
"EPOCH": "2026-07-07T04:58:23.082+00:00",
"MEAN_MOTION": 15.36806567,
"ECCENTRICITY": 0.0003261,
"INCLINATION": 97.6918,
"RA_OF_ASC_NODE": 0.1156,
"ARG_OF_PERICENTER": 70.4343,
"MEAN_ANOMALY": 289.7252,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 54685,
"REV_AT_EPOCH": 19852,
"BSTAR": 0.00025289,
"MEAN_MOTION_DOT": 0.00009011,
"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 09 |
| 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 |