View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64470U 26145.60201441 +.00000000 +00000-0 +00000-0 0 00000
2 64470 0.0372 105.6096 0003036 314.1113 132.4015 1.00272760 09
| Epoch (UTC): | 25 May 2026 14:26:54 |
| Eccentricity: | 0.0003036 |
| inclination: | 0.0372° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 105.6096° |
| argument of perigee: | 314.1113° |
| revolutions per day: | 1.00272760 |
| mean anomaly at epoch: | 132.4015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|