View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48472U 26145.46547623 +.00000000 +00000-0 +96913-3 0 00004
2 48472 53.0598 205.0455 0001912 353.4269 6.6697 15.11357187 06
| Epoch (UTC): | 25 May 2026 11:10:17 |
| Eccentricity: | 0.0001912 |
| inclination: | 53.0598° |
| perigee height: | 531 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 205.0455° |
| argument of perigee: | 353.4269° |
| revolutions per day: | 15.11357187 |
| mean anomaly at epoch: | 6.6697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|