View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59926U 26145.36510411 +.00000000 +00000-0 -24057-4 0 00006
2 59926 43.0039 259.1335 0002201 274.0526 86.0074 15.27560930 04
| Epoch (UTC): | 25 May 2026 08:45:44 |
| Eccentricity: | 0.0002201 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 259.1335° |
| argument of perigee: | 274.0526° |
| revolutions per day: | 15.27560930 |
| mean anomaly at epoch: | 86.0074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|