View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28654U 05018A 22177.90902303 .00000149 00000-0 10423-3 0 9991
2 28654 98.9488 248.3375 0013257 307.2859 52.7104 14.12746323881310
| Epoch (UTC): | 26 June 2022 21:48:59 |
| Eccentricity: | 0.0013257 |
| inclination: | 98.9488° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 248.3375° |
| argument of perigee: | 307.2859° |
| revolutions per day: | 14.12746323 |
| mean anomaly at epoch: | 52.7104° |
| orbit number at epoch: | 88131 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|