View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68364U 26145.15937359 +.00000000 +00000-0 +33957-3 0 00000
2 68364 82.2962 38.9165 0006691 114.9622 245.2328 15.57495081 08
| Epoch (UTC): | 25 May 2026 03:49:29 |
| Eccentricity: | 0.0006691 |
| inclination: | 82.2962° |
| perigee height: | 390 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 38.9165° |
| argument of perigee: | 114.9622° |
| revolutions per day: | 15.57495081 |
| mean anomaly at epoch: | 245.2328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|