View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59869U 26145.45790316 +.00000000 +00000-0 +90899-4 0 00002
2 59869 43.0001 204.7240 0001242 271.5988 88.4721 15.27572661 07
| Epoch (UTC): | 25 May 2026 10:59:22 |
| Eccentricity: | 0.0001242 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.7240° |
| argument of perigee: | 271.5988° |
| revolutions per day: | 15.27572661 |
| mean anomaly at epoch: | 88.4721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|