View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59964U 26145.48726957 +.00000000 +00000-0 +46563-4 0 00000
2 59964 53.1606 68.8703 0001280 86.1605 273.9542 15.30196612 01
| Epoch (UTC): | 25 May 2026 11:41:40 |
| Eccentricity: | 0.0001280 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.8703° |
| argument of perigee: | 86.1605° |
| revolutions per day: | 15.30196612 |
| mean anomaly at epoch: | 273.9542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|