View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12586U 26160.17346808 +.00000000 +00000-0 +19565-3 0 00006
2 12586 97.6202 205.4141 0012345 44.3195 315.9033 15.34660600 03
| Epoch (UTC): | 09 June 2026 04:09:47 |
| Eccentricity: | 0.0012345 |
| inclination: | 97.6202° |
| perigee height: | 453 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 205.4141° |
| argument of perigee: | 44.3195° |
| revolutions per day: | 15.34660600 |
| mean anomaly at epoch: | 315.9033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|