View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64028U 26145.64438067 +.00000000 +00000-0 +35520-3 0 00007
2 64028 70.0012 280.2434 0002620 270.1575 89.9284 14.98342044 01
| Epoch (UTC): | 25 May 2026 15:27:54 |
| Eccentricity: | 0.0002620 |
| inclination: | 70.0012° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 280.2434° |
| argument of perigee: | 270.1575° |
| revolutions per day: | 14.98342044 |
| mean anomaly at epoch: | 89.9284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|