View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59084U 26145.54482926 +.00000000 +00000-0 +14640-4 0 00006
2 59084 42.9987 236.8235 0001295 270.1394 89.9309 15.27572645 01
| Epoch (UTC): | 25 May 2026 13:04:33 |
| Eccentricity: | 0.0001295 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.8235° |
| argument of perigee: | 270.1394° |
| revolutions per day: | 15.27572645 |
| mean anomaly at epoch: | 89.9309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|