View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68627U 26145.43243728 +.00000000 +00000-0 +31803-3 0 00001
2 68627 60.0172 265.6471 0023464 357.3147 2.7803 15.23776016 05
| Epoch (UTC): | 25 May 2026 10:22:42 |
| Eccentricity: | 0.0023464 |
| inclination: | 60.0172° |
| perigee height: | 478 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 265.6471° |
| argument of perigee: | 357.3147° |
| revolutions per day: | 15.23776016 |
| mean anomaly at epoch: | 2.7803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|