View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57794U 26145.60571925 +.00000000 +00000-0 +22675-3 0 00003
2 57794 49.9725 247.5461 0014390 180.9682 179.1204 14.23145659 04
| Epoch (UTC): | 25 May 2026 14:32:14 |
| Eccentricity: | 0.0014390 |
| inclination: | 49.9725° |
| perigee height: | 804 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 247.5461° |
| argument of perigee: | 180.9682° |
| revolutions per day: | 14.23145659 |
| mean anomaly at epoch: | 179.1204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|