View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40037U 26156.68866549 +.00000000 +00000-0 +23978-3 0 00001
2 40037 97.9978 106.9953 0011512 347.2776 12.8152 14.95480833 08
| Epoch (UTC): | 05 June 2026 16:31:40 |
| Eccentricity: | 0.0011512 |
| inclination: | 97.9978° |
| perigee height: | 573 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 106.9953° |
| argument of perigee: | 347.2776° |
| revolutions per day: | 14.95480833 |
| mean anomaly at epoch: | 12.8152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|