View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59017U 26145.51501130 +.00000000 +00000-0 +18801-4 0 00001
2 59017 53.1620 67.2235 0001320 84.6229 275.4924 15.34389774 07
| Epoch (UTC): | 25 May 2026 12:21:36 |
| Eccentricity: | 0.0001320 |
| inclination: | 53.1620° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 67.2235° |
| argument of perigee: | 84.6229° |
| revolutions per day: | 15.34389774 |
| mean anomaly at epoch: | 275.4924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|