View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00053U 26046.17244841 +.00000000 +00000-0 +86941-3 0 00001
2 00053 47.2797 358.7167 0098270 74.3396 286.8210 12.17401624 06
| Epoch (UTC): | 15 February 2026 04:08:19 |
| Eccentricity: | 0.0098270 |
| inclination: | 47.2797° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 358.7167° |
| argument of perigee: | 74.3396° |
| revolutions per day: | 12.17401624 |
| mean anomaly at epoch: | 286.8210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|