View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67700U 26145.57202894 +.00000000 +00000-0 +52243-3 0 00007
2 67700 97.2847 257.1583 0000566 101.7961 258.3345 15.33445244 07
| Epoch (UTC): | 25 May 2026 13:43:43 |
| Eccentricity: | 0.0000566 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1583° |
| argument of perigee: | 101.7961° |
| revolutions per day: | 15.33445244 |
| mean anomaly at epoch: | 258.3345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|