View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10820U 26066.54104847 +.00000000 +00000-0 +23820-3 0 00005
2 10820 98.4533 263.0317 0008311 294.6170 65.4151 14.37986096 04
| Epoch (UTC): | 07 March 2026 12:59:06 |
| Eccentricity: | 0.0008311 |
| inclination: | 98.4533° |
| perigee height: | 759 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 263.0317° |
| argument of perigee: | 294.6170° |
| revolutions per day: | 14.37986096 |
| mean anomaly at epoch: | 65.4151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|