View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59289U 26144.93724991 +.00000000 +00000-0 +55849-3 0 00001
2 59289 49.9880 55.0804 0001859 170.0960 190.0046 15.57126574 04
| Epoch (UTC): | 24 May 2026 22:29:38 |
| Eccentricity: | 0.0001859 |
| inclination: | 49.9880° |
| perigee height: | 395 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 55.0804° |
| argument of perigee: | 170.0960° |
| revolutions per day: | 15.57126574 |
| mean anomaly at epoch: | 190.0046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|