View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61908U 26145.64797793 +.00000000 +00000-0 +26407-3 0 00009
2 61908 97.4136 218.6277 0013527 132.2230 228.0153 15.17056282 08
| Epoch (UTC): | 25 May 2026 15:33:05 |
| Eccentricity: | 0.0013527 |
| inclination: | 97.4136° |
| perigee height: | 505 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 218.6277° |
| argument of perigee: | 132.2230° |
| revolutions per day: | 15.17056282 |
| mean anomaly at epoch: | 228.0153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|