View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00059U 26046.12104735 +.00000000 +00000-0 +47878-4 0 00006
2 00059 28.2500 30.7484 0188865 11.0567 349.4054 13.53161577 03
| Epoch (UTC): | 15 February 2026 02:54:18 |
| Eccentricity: | 0.0188865 |
| inclination: | 28.2500° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 30.7484° |
| argument of perigee: | 11.0567° |
| revolutions per day: | 13.53161577 |
| mean anomaly at epoch: | 349.4054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|