View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56488U 26145.35429456 +.00000000 +00000-0 +11858-4 0 00007
2 56488 69.9994 271.2536 0002986 270.4969 89.5848 14.98331818 05
| Epoch (UTC): | 25 May 2026 08:30:11 |
| Eccentricity: | 0.0002986 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.2536° |
| argument of perigee: | 270.4969° |
| revolutions per day: | 14.98331818 |
| mean anomaly at epoch: | 89.5848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|