View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59012U 26145.53210236 +.00000000 +00000-0 -18448-4 0 00000
2 59012 53.1608 81.5199 0001116 97.2052 262.9076 15.30176660 06
| Epoch (UTC): | 25 May 2026 12:46:13 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.1608° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.5199° |
| argument of perigee: | 97.2052° |
| revolutions per day: | 15.30176660 |
| mean anomaly at epoch: | 262.9076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|