View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67806U 26145.06140446 +.00000000 +00000-0 +49924-3 0 00004
2 67806 97.2857 333.1370 0001729 94.0261 266.1179 15.33450260 09
| Epoch (UTC): | 25 May 2026 01:28:25 |
| Eccentricity: | 0.0001729 |
| inclination: | 97.2857° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.1370° |
| argument of perigee: | 94.0261° |
| revolutions per day: | 15.33450260 |
| mean anomaly at epoch: | 266.1179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|