View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68215U 26145.40178566 +.00000000 +00000-0 +67018-3 0 00005
2 68215 97.2868 20.8318 0001145 102.5728 257.5643 15.33455720 09
| Epoch (UTC): | 25 May 2026 09:38:34 |
| Eccentricity: | 0.0001145 |
| inclination: | 97.2868° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 20.8318° |
| argument of perigee: | 102.5728° |
| revolutions per day: | 15.33455720 |
| mean anomaly at epoch: | 257.5643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|