View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55423U 26145.55434296 +.00000000 +00000-0 +62158-6 0 00006
2 55423 69.9992 250.7337 0003135 269.8846 90.1954 14.98329463 04
| Epoch (UTC): | 25 May 2026 13:18:15 |
| Eccentricity: | 0.0003135 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.7337° |
| argument of perigee: | 269.8846° |
| revolutions per day: | 14.98329463 |
| mean anomaly at epoch: | 90.1954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|