View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68848U 26145.58335647 +.00000000 +00000-0 +42130-3 0 00009
2 68848 97.2853 160.2623 0000995 110.2169 71.1048 15.49178202 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000995 |
| inclination: | 97.2853° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.2623° |
| argument of perigee: | 110.2169° |
| revolutions per day: | 15.49178202 |
| mean anomaly at epoch: | 71.1048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|