View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28895U 05043F 22177.33343712 .00000719 00000-0 14488-3 0 9994
2 28895 98.1078 308.5752 0017948 112.2633 248.0475 14.64361495888719
| Epoch (UTC): | 26 June 2022 08:00:08 |
| Eccentricity: | 0.0017948 |
| inclination: | 98.1078° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 308.5752° |
| argument of perigee: | 112.2633° |
| revolutions per day: | 14.64361495 |
| mean anomaly at epoch: | 248.0475° |
| orbit number at epoch: | 88871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|