View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62917U 26145.56870052 +.00000000 +00000-0 +11720-2 0 00002
2 62917 43.0007 244.2191 0002417 261.1121 98.9473 15.70904282 00
| Epoch (UTC): | 25 May 2026 13:38:55 |
| Eccentricity: | 0.0002417 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 244.2191° |
| argument of perigee: | 261.1121° |
| revolutions per day: | 15.70904282 |
| mean anomaly at epoch: | 98.9473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|