View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59320U 26145.08219137 +.00000000 +00000-0 +44506-3 0 00003
2 59320 43.0004 68.0359 0001091 245.0116 115.0622 15.27762036 09
| Epoch (UTC): | 25 May 2026 01:58:21 |
| Eccentricity: | 0.0001091 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 68.0359° |
| argument of perigee: | 245.0116° |
| revolutions per day: | 15.27762036 |
| mean anomaly at epoch: | 115.0622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|