View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55833U 26145.64971888 +.00000000 +00000-0 +16771-3 0 00001
2 55833 87.8935 294.2148 0002070 86.9510 273.1857 13.14502603 02
| Epoch (UTC): | 25 May 2026 15:35:35 |
| Eccentricity: | 0.0002070 |
| inclination: | 87.8935° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2148° |
| argument of perigee: | 86.9510° |
| revolutions per day: | 13.14502603 |
| mean anomaly at epoch: | 273.1857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|