View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68770U 26145.58335647 +.00000000 +00000-0 -24924-1 0 00003
2 68770 97.2847 182.4315 0001508 82.2124 35.9934 15.61173698 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001508 |
| inclination: | 97.2847° |
| perigee height: | 383 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 182.4315° |
| argument of perigee: | 82.2124° |
| revolutions per day: | 15.61173698 |
| mean anomaly at epoch: | 35.9934° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|