View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57076U 26144.96900000 +.00000000 +00000-0 +99741-5 0 00004
2 57076 43.0057 25.5680 0001282 265.2545 94.8161 15.27576964 05
| Epoch (UTC): | 24 May 2026 23:15:21 |
| Eccentricity: | 0.0001282 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.5680° |
| argument of perigee: | 265.2545° |
| revolutions per day: | 15.27576964 |
| mean anomaly at epoch: | 94.8161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|