View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59000U 26145.10379079 +.00000000 +00000-0 +45809-3 0 00000
2 59000 53.1585 80.9956 0001111 94.0753 266.0375 15.30218428 05
| Epoch (UTC): | 25 May 2026 02:29:27 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.9956° |
| argument of perigee: | 94.0753° |
| revolutions per day: | 15.30218428 |
| mean anomaly at epoch: | 266.0375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|