View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55789U 26145.37214470 +.00000000 +00000-0 +86602-4 0 00009
2 55789 69.9999 11.0661 0002745 272.1769 87.9075 14.98338568 05
| Epoch (UTC): | 25 May 2026 08:55:53 |
| Eccentricity: | 0.0002745 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.0661° |
| argument of perigee: | 272.1769° |
| revolutions per day: | 14.98338568 |
| mean anomaly at epoch: | 87.9075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|