View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66170U 26145.47875144 +.00000000 +00000-0 +52093-3 0 00003
2 66170 53.1595 65.5248 0001143 86.6309 273.4824 15.34400341 06
| Epoch (UTC): | 25 May 2026 11:29:24 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 65.5248° |
| argument of perigee: | 86.6309° |
| revolutions per day: | 15.34400341 |
| mean anomaly at epoch: | 273.4824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|