View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68564U 26145.62011439 +.00000000 +00000-0 +73640-3 0 00009
2 68564 53.1593 4.4822 0001103 81.0705 279.0422 15.34421490 02
| Epoch (UTC): | 25 May 2026 14:52:57 |
| Eccentricity: | 0.0001103 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 4.4822° |
| argument of perigee: | 81.0705° |
| revolutions per day: | 15.34421490 |
| mean anomaly at epoch: | 279.0422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|