View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28376U 04026A 23090.60166263 .00002509 00000-0 56430-3 0 9999
2 28376 98.2418 35.2931 0001768 71.8291 288.3100 14.57312955995088
| Epoch (UTC): | 31 March 2023 14:26:23 |
| Eccentricity: | 0.0001768 |
| inclination: | 98.2418° |
| perigee height: | 700 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 35.2931° |
| argument of perigee: | 71.8291° |
| revolutions per day: | 14.57312955 |
| mean anomaly at epoch: | 288.3100° |
| orbit number at epoch: | 99508 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|