View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59391U 26145.66668980 +.00000000 +00000-0 +25505-2 0 00006
2 59391 53.1584 260.6368 0002037 118.0511 163.8002 15.34296278 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0002037 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 260.6368° |
| argument of perigee: | 118.0511° |
| revolutions per day: | 15.34296278 |
| mean anomaly at epoch: | 163.8002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|