View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66358U 26145.54148372 +.00000000 +00000-0 +97322-3 0 00009
2 66358 53.1576 235.3710 0000917 73.0892 287.0210 15.31720962 00
| Epoch (UTC): | 25 May 2026 12:59:44 |
| Eccentricity: | 0.0000917 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.3710° |
| argument of perigee: | 73.0892° |
| revolutions per day: | 15.31720962 |
| mean anomaly at epoch: | 287.0210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|