View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58960U 26145.62309840 +.00000000 +00000-0 +35490-3 0 00005
2 58960 39.9889 247.8028 0010040 32.3621 327.7784 14.95113939 02
| Epoch (UTC): | 25 May 2026 14:57:15 |
| Eccentricity: | 0.0010040 |
| inclination: | 39.9889° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 247.8028° |
| argument of perigee: | 32.3621° |
| revolutions per day: | 14.95113939 |
| mean anomaly at epoch: | 327.7784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|