View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64202U 26145.40733330 +.00000000 +00000-0 +00000-0 0 00008
2 64202 55.2192 32.0466 0008614 335.9323 206.6816 2.00577585 06
| Epoch (UTC): | 25 May 2026 09:46:33 |
| Eccentricity: | 0.0008614 |
| inclination: | 55.2192° |
| perigee height: | 20158 km |
| apogee height: | 20204 km |
| right ascension of ascending node: | 32.0466° |
| argument of perigee: | 335.9323° |
| revolutions per day: | 2.00577585 |
| mean anomaly at epoch: | 206.6816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|