View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68269U 26145.20112855 +.00000000 +00000-0 +60881-3 0 00002
2 68269 53.1584 322.5490 0001188 77.3689 282.7447 15.34412648 04
| Epoch (UTC): | 25 May 2026 04:49:37 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 322.5490° |
| argument of perigee: | 77.3689° |
| revolutions per day: | 15.34412648 |
| mean anomaly at epoch: | 282.7447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|