View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60056U 26145.50003470 +.00000000 +00000-0 -64076-3 0 00004
2 60056 53.1581 81.4240 0001477 92.2754 271.4172 15.30201288 03
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001477 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.4240° |
| argument of perigee: | 92.2754° |
| revolutions per day: | 15.30201288 |
| mean anomaly at epoch: | 271.4172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|