View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59181U 26145.35329355 +.00000000 +00000-0 +65908-4 0 00002
2 59181 42.9981 16.3417 0000089 318.3687 41.7158 15.27573140 05
| Epoch (UTC): | 25 May 2026 08:28:44 |
| Eccentricity: | 0.0000089 |
| inclination: | 42.9981° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 16.3417° |
| argument of perigee: | 318.3687° |
| revolutions per day: | 15.27573140 |
| mean anomaly at epoch: | 41.7158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|