View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00058U 26044.36608588 +.00000000 +00000-0 +27027-4 0 00008
2 00058 28.3294 48.0182 0164765 262.4806 95.6993 13.46424363 00
| Epoch (UTC): | 13 February 2026 08:47:09 |
| Eccentricity: | 0.0164765 |
| inclination: | 28.3294° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 48.0182° |
| argument of perigee: | 262.4806° |
| revolutions per day: | 13.46424363 |
| mean anomaly at epoch: | 95.6993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|