View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27940U 26017.21143147 +.00000000 +00000-0 +10306-3 0 00007
2 27940 98.3743 191.2388 0014096 111.0536 249.2178 14.69262153 09
| Epoch (UTC): | 17 January 2026 05:04:27 |
| Eccentricity: | 0.0014096 |
| inclination: | 98.3743° |
| perigee height: | 653 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 191.2388° |
| argument of perigee: | 111.0536° |
| revolutions per day: | 14.69262153 |
| mean anomaly at epoch: | 249.2178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|