View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42961U 26145.61683228 +.00000000 +00000-0 +49321-4 0 00002
2 42961 86.3990 34.6847 0002265 84.7069 275.4385 14.34217580 09
| Epoch (UTC): | 25 May 2026 14:48:14 |
| Eccentricity: | 0.0002265 |
| inclination: | 86.3990° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.6847° |
| argument of perigee: | 84.7069° |
| revolutions per day: | 14.34217580 |
| mean anomaly at epoch: | 275.4385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|