View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55152U 26145.50377727 +.00000000 +00000-0 +11822-3 0 00004
2 55152 87.9161 339.9853 0001248 114.7133 245.4129 13.18686472 00
| Epoch (UTC): | 25 May 2026 12:05:26 |
| Eccentricity: | 0.0001248 |
| inclination: | 87.9161° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9853° |
| argument of perigee: | 114.7133° |
| revolutions per day: | 13.18686472 |
| mean anomaly at epoch: | 245.4129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|