HONGYAN 1 (CHONGQING) is a payload in LEO orbit, operated by Shenzhen Hangtian DongFangHong Weixing Yidong Tongxin YG, launched 2018.
| Orbit class | LEO |
| Inclination | 50.0071° |
| Eccentricity | 0.0006727 |
| Period | 107.2 min |
| Apogee | 1,100 km |
| Perigee | 1,090 km |
| Mean motion | 13.43821684 rev/day |
| RAAN | 165.7064° |
| Arg of perigee | 315.9646° |
| Mean anomaly | 44.0696° |
| B* | -2.9722e-5 |
| Rev at epoch | 36,914 |
1 43914U 18112F 26187.57416632 -.00000146 00000-0 -29722-4 0 99912 43914 50.0071 165.7064 0006727 315.9646 44.0696 13.43821684369143{
"OBJECT_NAME": "HONGYAN 1 (CHONGQING)",
"OBJECT_ID": "2018-112F",
"EPOCH": "2026-07-06T13:46:47.97+00:00",
"MEAN_MOTION": 13.43821684,
"ECCENTRICITY": 0.0006727,
"INCLINATION": 50.0071,
"RA_OF_ASC_NODE": 165.7064,
"ARG_OF_PERICENTER": 315.9646,
"MEAN_ANOMALY": 44.0696,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 43914,
"REV_AT_EPOCH": 36914,
"BSTAR": -0.000029722,
"MEAN_MOTION_DOT": -0.00000146,
"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 | HONGYAN 1 (CHONGQING) |
| Operator | Shenzhen Hangtian DongFangHong Weixing Yidong Tongxin YGHIGHvia 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 |