View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59491U 26145.38732876 +.00000000 +00000-0 +10295-2 0 00002
2 59491 42.9999 278.0067 0001402 288.2627 71.8072 15.27606927 04
| Epoch (UTC): | 25 May 2026 09:17:45 |
| Eccentricity: | 0.0001402 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 278.0067° |
| argument of perigee: | 288.2627° |
| revolutions per day: | 15.27606927 |
| mean anomaly at epoch: | 71.8072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|