View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64823U 26145.48206101 +.00000000 +00000-0 +17873-3 0 00005
2 64823 51.9020 313.5184 0001050 134.1620 225.9429 14.79934459 08
| Epoch (UTC): | 25 May 2026 11:34:10 |
| Eccentricity: | 0.0001050 |
| inclination: | 51.9020° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 313.5184° |
| argument of perigee: | 134.1620° |
| revolutions per day: | 14.79934459 |
| mean anomaly at epoch: | 225.9429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|