View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60235U 26137.53154035 +.00000000 +00000-0 +12411-3 0 00006
2 60235 61.9949 337.8620 0054225 128.6068 231.9896 15.00982218 08
| Epoch (UTC): | 17 May 2026 12:45:25 |
| Eccentricity: | 0.0054225 |
| inclination: | 61.9949° |
| perigee height: | 526 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 337.8620° |
| argument of perigee: | 128.6068° |
| revolutions per day: | 15.00982218 |
| mean anomaly at epoch: | 231.9896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|