View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57901U 26145.55504287 +.00000000 +00000-0 +76302-4 0 00001
2 57901 42.9994 236.5376 0001257 276.6390 83.4318 15.27585548 08
| Epoch (UTC): | 25 May 2026 13:19:15 |
| Eccentricity: | 0.0001257 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.5376° |
| argument of perigee: | 276.6390° |
| revolutions per day: | 15.27585548 |
| mean anomaly at epoch: | 83.4318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|