View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43479U 26145.35729500 +.00000000 +00000-0 -28660-4 0 00006
2 43479 86.3947 97.8773 0002278 87.4847 272.6610 14.34217324 09
| Epoch (UTC): | 25 May 2026 08:34:30 |
| Eccentricity: | 0.0002278 |
| inclination: | 86.3947° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.8773° |
| argument of perigee: | 87.4847° |
| revolutions per day: | 14.34217324 |
| mean anomaly at epoch: | 272.6610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|