View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 09510U 26139.91462750 +.00000000 +00000-0 -47341-4 0 00007
2 09510 82.9345 118.4409 0027320 55.4072 304.9657 13.77885377 02
| Epoch (UTC): | 19 May 2026 21:57:03 |
| Eccentricity: | 0.0027320 |
| inclination: | 82.9345° |
| perigee height: | 951 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 118.4409° |
| argument of perigee: | 55.4072° |
| revolutions per day: | 13.77885377 |
| mean anomaly at epoch: | 304.9657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|