View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20797U 26100.18999167 +.00000000 +00000-0 +42215-3 0 00004
2 20797 98.8035 86.8701 0008162 335.8853 86.6361 14.18284224 08
| Epoch (UTC): | 10 April 2026 04:33:35 |
| Eccentricity: | 0.0008162 |
| inclination: | 98.8035° |
| perigee height: | 825 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 86.8701° |
| argument of perigee: | 335.8853° |
| revolutions per day: | 14.18284224 |
| mean anomaly at epoch: | 86.6361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|