View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59308U 26145.46891927 +.00000000 +00000-0 +32725-4 0 00005
2 59308 43.0000 157.3622 0000993 275.5633 84.5105 15.27575368 04
| Epoch (UTC): | 25 May 2026 11:15:14 |
| Eccentricity: | 0.0000993 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.3622° |
| argument of perigee: | 275.5633° |
| revolutions per day: | 15.27575368 |
| mean anomaly at epoch: | 84.5105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|