View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53051U 26145.39565023 +.00000000 +00000-0 +79865-4 0 00007
2 53051 97.4471 325.2639 0000863 132.7835 227.3465 15.05661812 08
| Epoch (UTC): | 25 May 2026 09:29:44 |
| Eccentricity: | 0.0000863 |
| inclination: | 97.4471° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.2639° |
| argument of perigee: | 132.7835° |
| revolutions per day: | 15.05661812 |
| mean anomaly at epoch: | 227.3465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|