View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57582U 26145.61647530 +.00000000 +00000-0 +52463-3 0 00003
2 57582 97.4071 226.3563 0005065 321.5517 38.5367 15.39515865 04
| Epoch (UTC): | 25 May 2026 14:47:43 |
| Eccentricity: | 0.0005065 |
| inclination: | 97.4071° |
| perigee height: | 444 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 226.3563° |
| argument of perigee: | 321.5517° |
| revolutions per day: | 15.39515865 |
| mean anomaly at epoch: | 38.5367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|