View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59784U 26145.44002082 +.00000000 +00000-0 -46792-4 0 00007
2 59784 43.0022 131.9676 0000998 246.0238 114.0510 15.27575360 03
| Epoch (UTC): | 25 May 2026 10:33:37 |
| Eccentricity: | 0.0000998 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.9676° |
| argument of perigee: | 246.0238° |
| revolutions per day: | 15.27575360 |
| mean anomaly at epoch: | 114.0510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|