View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55302U 26145.54528898 +.00000000 +00000-0 +76939-4 0 00003
2 55302 69.9988 190.5796 0003458 268.8790 91.1972 14.98331474 06
| Epoch (UTC): | 25 May 2026 13:05:12 |
| Eccentricity: | 0.0003458 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 190.5796° |
| argument of perigee: | 268.8790° |
| revolutions per day: | 14.98331474 |
| mean anomaly at epoch: | 91.1972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|