View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56465U 26145.38348652 +.00000000 +00000-0 -12830-4 0 00005
2 56465 69.9992 270.9207 0003154 270.6761 89.4037 14.98329076 01
| Epoch (UTC): | 25 May 2026 09:12:13 |
| Eccentricity: | 0.0003154 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.9207° |
| argument of perigee: | 270.6761° |
| revolutions per day: | 14.98329076 |
| mean anomaly at epoch: | 89.4037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|