View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17528U 26100.00414873 +.00000000 +00000-0 +11685-3 0 00006
2 17528 97.4038 101.9838 0142567 274.3462 84.1459 14.54546178 05
| Epoch (UTC): | 10 April 2026 00:05:58 |
| Eccentricity: | 0.0142567 |
| inclination: | 97.4038° |
| perigee height: | 610 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 101.9838° |
| argument of perigee: | 274.3462° |
| revolutions per day: | 14.54546178 |
| mean anomaly at epoch: | 84.1459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|