View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54518U 26088.05623683 +.00000000 +00000-0 +37397-3 0 00005
2 54518 98.7798 127.1002 0126229 350.2612 9.6125 14.29914414 09
| Epoch (UTC): | 29 March 2026 01:20:58 |
| Eccentricity: | 0.0126229 |
| inclination: | 98.7798° |
| perigee height: | 702 km |
| apogee height: | 883 km |
| right ascension of ascending node: | 127.1002° |
| argument of perigee: | 350.2612° |
| revolutions per day: | 14.29914414 |
| mean anomaly at epoch: | 9.6125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|