View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65820U 26145.47705847 +.00000000 +00000-0 +91226-4 0 00008
2 65820 86.5005 51.5578 0001436 62.9532 297.1748 13.24405064 06
| Epoch (UTC): | 25 May 2026 11:26:57 |
| Eccentricity: | 0.0001436 |
| inclination: | 86.5005° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 51.5578° |
| argument of perigee: | 62.9532° |
| revolutions per day: | 13.24405064 |
| mean anomaly at epoch: | 297.1748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|