View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56487U 26145.37933177 +.00000000 +00000-0 -22748-6 0 00001
2 56487 69.9988 270.9430 0003198 269.1361 90.9432 14.98321764 07
| Epoch (UTC): | 25 May 2026 09:06:14 |
| Eccentricity: | 0.0003198 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.9430° |
| argument of perigee: | 269.1361° |
| revolutions per day: | 14.98321764 |
| mean anomaly at epoch: | 90.9432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|