View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56451U 26145.20872834 +.00000000 +00000-0 +34417-4 0 00009
2 56451 69.9987 311.6924 0003067 266.3834 93.6974 14.98338964 08
| Epoch (UTC): | 25 May 2026 05:00:34 |
| Eccentricity: | 0.0003067 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 311.6924° |
| argument of perigee: | 266.3834° |
| revolutions per day: | 14.98338964 |
| mean anomaly at epoch: | 93.6974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|