DONGPO 03 is a payload in SSO orbit, operated by Chang Guang Satellite Technology Ltd, launched 2022.
Orbital data last updated 46 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | SSO |
| Inclination | 97.5516° |
| Eccentricity | 0.0004451 |
| Period | 90.2 min |
| Apogee | 285 km |
| Perigee | 279 km |
| Mean motion | 15.97334439 rev/day |
| RAAN | 277.5264° |
| Arg of perigee | 240.2200° |
| Mean anomaly | 119.8634° |
| B* | 8.1357e-4 |
| Rev at epoch | 21,103 |
This object is recorded as DECAYED (re-entered). These are the last known elements before re-entry — not a current orbit.
1 53450U 22098G 26142.07466683 .00354972 53400-4 81357-3 0 99962 53450 97.5516 277.5264 0004451 240.2200 119.8634 15.97334439211036{
"OBJECT_NAME": "DONGPO 03",
"OBJECT_ID": "2022-098G",
"EPOCH": "2026-05-22T01:47:31.214+00:00",
"MEAN_MOTION": 15.97334439,
"ECCENTRICITY": 0.0004451,
"INCLINATION": 97.5516,
"RA_OF_ASC_NODE": 277.5264,
"ARG_OF_PERICENTER": 240.22,
"MEAN_ANOMALY": 119.8634,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 53450,
"REV_AT_EPOCH": 21103,
"BSTAR": 0.00081357123,
"MEAN_MOTION_DOT": 0.00354972,
"MEAN_MOTION_DDOT": 0.000053399701
}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 03 |
| 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 |
| Decay date |