View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55372U 26145.54397175 +.00000000 +00000-0 +23737-4 0 00000
2 55372 43.0034 244.3707 0001522 272.3756 87.6921 15.27573967 02
| Epoch (UTC): | 25 May 2026 13:03:19 |
| Eccentricity: | 0.0001522 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 244.3707° |
| argument of perigee: | 272.3756° |
| revolutions per day: | 15.27573967 |
| mean anomaly at epoch: | 87.6921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|