View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54670U 26145.52659471 +.00000000 +00000-0 +14313-3 0 00007
2 54670 87.9252 248.5084 0001835 102.9638 257.1701 13.21824807 03
| Epoch (UTC): | 25 May 2026 12:38:17 |
| Eccentricity: | 0.0001835 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5084° |
| argument of perigee: | 102.9638° |
| revolutions per day: | 13.21824807 |
| mean anomaly at epoch: | 257.1701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|