View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59644U 26145.12760987 +.00000000 +00000-0 +51920-3 0 00009
2 59644 43.0003 67.9936 0001531 266.4946 93.5730 15.27595355 01
| Epoch (UTC): | 25 May 2026 03:03:45 |
| Eccentricity: | 0.0001531 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.9936° |
| argument of perigee: | 266.4946° |
| revolutions per day: | 15.27595355 |
| mean anomaly at epoch: | 93.5730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|