View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62698U 26145.46937103 +.00000000 +00000-0 +17883-3 0 00005
2 62698 97.7398 224.1922 0001769 99.8813 260.2605 14.91869081 07
| Epoch (UTC): | 25 May 2026 11:15:53 |
| Eccentricity: | 0.0001769 |
| inclination: | 97.7398° |
| perigee height: | 591 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 224.1922° |
| argument of perigee: | 99.8813° |
| revolutions per day: | 14.91869081 |
| mean anomaly at epoch: | 260.2605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|