View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68289U 26145.50164810 +.00000000 +00000-0 +12661-2 0 00007
2 68289 53.1592 321.5805 0001171 105.5274 254.5858 15.34426546 05
| Epoch (UTC): | 25 May 2026 12:02:22 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 321.5805° |
| argument of perigee: | 105.5274° |
| revolutions per day: | 15.34426546 |
| mean anomaly at epoch: | 254.5858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|