View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59879U 26145.13236744 +.00000000 +00000-0 +44431-4 0 00009
2 59879 43.0031 195.7837 0002601 275.5338 84.5217 15.27565295 07
| Epoch (UTC): | 25 May 2026 03:10:36 |
| Eccentricity: | 0.0002601 |
| inclination: | 43.0031° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 195.7837° |
| argument of perigee: | 275.5338° |
| revolutions per day: | 15.27565295 |
| mean anomaly at epoch: | 84.5217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|