View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62920U 26145.45204448 +.00000000 +00000-0 +80800-3 0 00000
2 62920 43.0013 55.2306 0001275 260.4517 99.6191 15.27611003 04
| Epoch (UTC): | 25 May 2026 10:50:56 |
| Eccentricity: | 0.0001275 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.2306° |
| argument of perigee: | 260.4517° |
| revolutions per day: | 15.27611003 |
| mean anomaly at epoch: | 99.6191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|