View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53665U 26145.66668980 +.00000000 +00000-0 +22594-2 0 00009
2 53665 97.6028 28.8334 0002083 71.3672 36.5376 15.37950877 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0002083 |
| inclination: | 97.6028° |
| perigee height: | 451 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 28.8334° |
| argument of perigee: | 71.3672° |
| revolutions per day: | 15.37950877 |
| mean anomaly at epoch: | 36.5376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|