View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00107U 26149.15077985 +.00000000 +00000-0 +26548-3 0 00003
2 00107 28.7813 66.2021 0493717 310.5014 45.3531 14.22031388 04
| Epoch (UTC): | 29 May 2026 03:37:07 |
| Eccentricity: | 0.0493717 |
| inclination: | 28.7813° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 66.2021° |
| argument of perigee: | 310.5014° |
| revolutions per day: | 14.22031388 |
| mean anomaly at epoch: | 45.3531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|