View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63059U 26145.40529442 +.00000000 +00000-0 +15079-2 0 00008
2 63059 43.0048 273.1554 0002157 259.9959 100.0666 15.70954280 04
| Epoch (UTC): | 25 May 2026 09:43:37 |
| Eccentricity: | 0.0002157 |
| inclination: | 43.0048° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 273.1554° |
| argument of perigee: | 259.9959° |
| revolutions per day: | 15.70954280 |
| mean anomaly at epoch: | 100.0666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|