View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68403U 26145.65675873 +.00000000 +00000-0 +10356-2 0 00006
2 68403 97.2852 289.3296 0002944 90.6687 269.4915 15.75242036 01
| Epoch (UTC): | 25 May 2026 15:45:43 |
| Eccentricity: | 0.0002944 |
| inclination: | 97.2852° |
| perigee height: | 342 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 289.3296° |
| argument of perigee: | 90.6687° |
| revolutions per day: | 15.75242036 |
| mean anomaly at epoch: | 269.4915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|