View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43181U 26150.50257090 +.00000000 +00000-0 +14911-3 0 00001
2 43181 97.3611 56.5387 0001991 81.5066 278.6396 15.22878659 00
| Epoch (UTC): | 30 May 2026 12:03:42 |
| Eccentricity: | 0.0001991 |
| inclination: | 97.3611° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 56.5387° |
| argument of perigee: | 81.5066° |
| revolutions per day: | 15.22878659 |
| mean anomaly at epoch: | 278.6396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|