View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59621U 26145.49714269 +.00000000 +00000-0 +20401-3 0 00006
2 59621 42.9994 320.3094 0001255 272.0457 88.0251 15.27596203 07
| Epoch (UTC): | 25 May 2026 11:55:53 |
| Eccentricity: | 0.0001255 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.3094° |
| argument of perigee: | 272.0457° |
| revolutions per day: | 15.27596203 |
| mean anomaly at epoch: | 88.0251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|