View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56462U 26145.37530131 +.00000000 +00000-0 +24978-4 0 00001
2 56462 69.9988 270.8963 0003280 268.9250 91.1533 14.98329476 09
| Epoch (UTC): | 25 May 2026 09:00:26 |
| Eccentricity: | 0.0003280 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.8963° |
| argument of perigee: | 268.9250° |
| revolutions per day: | 14.98329476 |
| mean anomaly at epoch: | 91.1533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|