View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55574U 26145.42090007 +.00000000 +00000-0 +16599-4 0 00003
2 55574 43.0042 295.6366 0002316 261.6849 98.3740 15.27570095 08
| Epoch (UTC): | 25 May 2026 10:06:05 |
| Eccentricity: | 0.0002316 |
| inclination: | 43.0042° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 295.6366° |
| argument of perigee: | 261.6849° |
| revolutions per day: | 15.27570095 |
| mean anomaly at epoch: | 98.3740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|