View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47828U 26145.57480106 +.00000000 +00000-0 +11940-4 0 00000
2 47828 53.1592 257.7037 0001191 93.0821 267.0316 15.31704174 00
| Epoch (UTC): | 25 May 2026 13:47:42 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 257.7037° |
| argument of perigee: | 93.0821° |
| revolutions per day: | 15.31704174 |
| mean anomaly at epoch: | 267.0316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|