View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68578U 26145.12081870 +.00000000 +00000-0 +31035-3 0 00007
2 68578 51.9016 297.2024 0002294 135.3207 224.7939 14.76350272 05
| Epoch (UTC): | 25 May 2026 02:53:58 |
| Eccentricity: | 0.0002294 |
| inclination: | 51.9016° |
| perigee height: | 639 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 297.2024° |
| argument of perigee: | 135.3207° |
| revolutions per day: | 14.76350272 |
| mean anomaly at epoch: | 224.7939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|