View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68614U 26145.58335647 +.00000000 +00000-0 -28236-1 0 00000
2 68614 97.2849 345.1283 0001909 83.6471 140.1018 15.58198413 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001909 |
| inclination: | 97.2849° |
| perigee height: | 392 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 345.1283° |
| argument of perigee: | 83.6471° |
| revolutions per day: | 15.58198413 |
| mean anomaly at epoch: | 140.1018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|