View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41328U 26144.93347675 +.00000000 +00000-0 +00000-0 0 00002
2 41328 55.5105 90.3811 0096100 247.3195 111.6364 2.00552846 04
| Epoch (UTC): | 24 May 2026 22:24:12 |
| Eccentricity: | 0.0096100 |
| inclination: | 55.5105° |
| perigee height: | 19928 km |
| apogee height: | 20438 km |
| right ascension of ascending node: | 90.3811° |
| argument of perigee: | 247.3195° |
| revolutions per day: | 2.00552846 |
| mean anomaly at epoch: | 111.6364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|