View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21575U 26110.18256970 +.00000000 +00000-0 +49102-4 0 00001
2 21575 98.3533 179.8624 0006963 0.4618 359.6577 14.42346855 07
| Epoch (UTC): | 20 April 2026 04:22:54 |
| Eccentricity: | 0.0006963 |
| inclination: | 98.3533° |
| perigee height: | 746 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 179.8624° |
| argument of perigee: | 0.4618° |
| revolutions per day: | 14.42346855 |
| mean anomaly at epoch: | 359.6577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|