View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47952U 21022W 25157.69972699 .06655353 25454-5 93288-3 0 9992
2 47952 97.3980 72.5414 0010307 219.3637 140.6911 16.34906352233436
| Epoch (UTC): | 06 June 2025 16:47:36 |
| Eccentricity: | 0.0010307 |
| inclination: | 97.3980° |
| perigee height: | 172 km |
| apogee height: | 186 km |
| right ascension of ascending node: | 72.5414° |
| argument of perigee: | 219.3637° |
| revolutions per day: | 16.34906352 |
| mean anomaly at epoch: | 140.6911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|