View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68155U 26145.30435711 +.00000000 +00000-0 +24024-3 0 00005
2 68155 97.2860 166.8834 0000334 141.9545 218.1722 15.33435232 08
| Epoch (UTC): | 25 May 2026 07:18:16 |
| Eccentricity: | 0.0000334 |
| inclination: | 97.2860° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.8834° |
| argument of perigee: | 141.9545° |
| revolutions per day: | 15.33435232 |
| mean anomaly at epoch: | 218.1722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|