View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40975U 26145.42094438 +.00000000 +00000-0 +37223-3 0 00000
2 40975 64.7652 291.7899 0105261 64.8259 296.3730 15.02041858 05
| Epoch (UTC): | 25 May 2026 10:06:09 |
| Eccentricity: | 0.0105261 |
| inclination: | 64.7652° |
| perigee height: | 488 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 291.7899° |
| argument of perigee: | 64.8259° |
| revolutions per day: | 15.02041858 |
| mean anomaly at epoch: | 296.3730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|