View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60598U 26145.48371154 +.00000000 +00000-0 +34130-4 0 00007
2 60598 53.1605 310.6991 0001009 97.0486 263.0629 15.30196998 02
| Epoch (UTC): | 25 May 2026 11:36:32 |
| Eccentricity: | 0.0001009 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6991° |
| argument of perigee: | 97.0486° |
| revolutions per day: | 15.30196998 |
| mean anomaly at epoch: | 263.0629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|