View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59950U 26145.53609316 +.00000000 +00000-0 +12280-4 0 00009
2 59950 53.1599 232.5786 0000573 47.3273 312.7793 15.69698045 01
| Epoch (UTC): | 25 May 2026 12:51:58 |
| Eccentricity: | 0.0000573 |
| inclination: | 53.1599° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 232.5786° |
| argument of perigee: | 47.3273° |
| revolutions per day: | 15.69698045 |
| mean anomaly at epoch: | 312.7793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|