View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60235U 26137.59815877 +.00000000 +00000-0 +12379-3 0 00003
2 60235 61.9949 337.6303 0054219 128.6245 231.9718 15.00982405 05
| Epoch (UTC): | 17 May 2026 14:21:20 |
| Eccentricity: | 0.0054219 |
| inclination: | 61.9949° |
| perigee height: | 526 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 337.6303° |
| argument of perigee: | 128.6245° |
| revolutions per day: | 15.00982405 |
| mean anomaly at epoch: | 231.9718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|