View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27640U 26075.88723554 +.00000000 +00000-0 +86338-4 0 00006
2 27640 98.7159 84.1714 0015046 117.0946 243.1767 14.19915738 07
| Epoch (UTC): | 16 March 2026 21:17:37 |
| Eccentricity: | 0.0015046 |
| inclination: | 98.7159° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 84.1714° |
| argument of perigee: | 117.0946° |
| revolutions per day: | 14.19915738 |
| mean anomaly at epoch: | 243.1767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|