View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54254U 26145.58474406 +.00000000 +00000-0 +70407-3 0 00000
2 54254 97.6103 295.9011 0000644 217.5251 142.5975 15.86377805 05
| Epoch (UTC): | 25 May 2026 14:02:01 |
| Eccentricity: | 0.0000644 |
| inclination: | 97.6103° |
| perigee height: | 312 km |
| apogee height: | 313 km |
| right ascension of ascending node: | 295.9011° |
| argument of perigee: | 217.5251° |
| revolutions per day: | 15.86377805 |
| mean anomaly at epoch: | 142.5975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|