View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57151U 26145.52802221 +.00000000 +00000-0 +15597-1 0 00000
2 57151 43.0021 189.4884 0000966 305.5955 54.4807 15.28556553 09
| Epoch (UTC): | 25 May 2026 12:40:21 |
| Eccentricity: | 0.0000966 |
| inclination: | 43.0021° |
| perigee height: | 479 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 189.4884° |
| argument of perigee: | 305.5955° |
| revolutions per day: | 15.28556553 |
| mean anomaly at epoch: | 54.4807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|