View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59908U 26145.30316970 +.00000000 +00000-0 +16165-3 0 00003
2 59908 97.0486 272.1518 0001560 101.9282 258.2149 15.57096966 03
| Epoch (UTC): | 25 May 2026 07:16:33 |
| Eccentricity: | 0.0001560 |
| inclination: | 97.0486° |
| perigee height: | 395 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 272.1518° |
| argument of perigee: | 101.9282° |
| revolutions per day: | 15.57096966 |
| mean anomaly at epoch: | 258.2149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|