View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55836U 26145.58922748 +.00000000 +00000-0 +26513-3 0 00003
2 55836 99.0136 154.0981 0002288 58.8151 301.3238 14.01350281 08
| Epoch (UTC): | 25 May 2026 14:08:29 |
| Eccentricity: | 0.0002288 |
| inclination: | 99.0136° |
| perigee height: | 887 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 154.0981° |
| argument of perigee: | 58.8151° |
| revolutions per day: | 14.01350281 |
| mean anomaly at epoch: | 301.3238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|