View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27453U 26161.63162149 +.00000000 +00000-0 +80984-4 0 00005
2 27453 98.8649 127.3282 0011998 16.2824 343.8738 14.26234454 04
| Epoch (UTC): | 10 June 2026 15:09:32 |
| Eccentricity: | 0.0011998 |
| inclination: | 98.8649° |
| perigee height: | 796 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 127.3282° |
| argument of perigee: | 16.2824° |
| revolutions per day: | 14.26234454 |
| mean anomaly at epoch: | 343.8738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|