View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27875U 26139.88493632 +.00000000 +00000-0 +00000-0 0 00006
2 27875 10.4426 48.2161 0001754 12.1827 159.8211 1.00273158 02
| Epoch (UTC): | 19 May 2026 21:14:18 |
| Eccentricity: | 0.0001754 |
| inclination: | 10.4426° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 48.2161° |
| argument of perigee: | 12.1827° |
| revolutions per day: | 1.00273158 |
| mean anomaly at epoch: | 159.8211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|