View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60013U 26145.62044124 +.00000000 +00000-0 +29722-3 0 00009
2 60013 97.5712 241.4149 0009997 335.3447 24.7310 15.22103589 04
| Epoch (UTC): | 25 May 2026 14:53:26 |
| Eccentricity: | 0.0009997 |
| inclination: | 97.5712° |
| perigee height: | 493 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 241.4149° |
| argument of perigee: | 335.3447° |
| revolutions per day: | 15.22103589 |
| mean anomaly at epoch: | 24.7310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|