View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25940U 26106.97230352 +.00000000 +00000-0 +46420-4 0 00009
2 25940 98.8511 114.8039 0005092 166.2181 193.9144 14.36979766 00
| Epoch (UTC): | 16 April 2026 23:20:07 |
| Eccentricity: | 0.0005092 |
| inclination: | 98.8511° |
| perigee height: | 765 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 114.8039° |
| argument of perigee: | 166.2181° |
| revolutions per day: | 14.36979766 |
| mean anomaly at epoch: | 193.9144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|