View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36597U 26017.30140660 +.00000000 +00000-0 +10846-3 0 00001
2 36597 97.9924 41.9878 0052659 66.4659 294.2085 15.01943893 05
| Epoch (UTC): | 17 January 2026 07:14:01 |
| Eccentricity: | 0.0052659 |
| inclination: | 97.9924° |
| perigee height: | 524 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 41.9878° |
| argument of perigee: | 66.4659° |
| revolutions per day: | 15.01943893 |
| mean anomaly at epoch: | 294.2085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|