View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50493U 26145.50194764 +.00000000 +00000-0 +10389-3 0 00002
2 50493 87.9169 339.9705 0002033 95.0947 265.0417 13.18685125 06
| Epoch (UTC): | 25 May 2026 12:02:48 |
| Eccentricity: | 0.0002033 |
| inclination: | 87.9169° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9705° |
| argument of perigee: | 95.0947° |
| revolutions per day: | 13.18685125 |
| mean anomaly at epoch: | 265.0417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|