View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40018U 26053.63071404 +.00000000 +00000-0 +15214-3 0 00003
2 40018 97.8857 189.7664 0065776 207.6192 152.1517 14.74034002 05
| Epoch (UTC): | 22 February 2026 15:08:13 |
| Eccentricity: | 0.0065776 |
| inclination: | 97.8857° |
| perigee height: | 602 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 189.7664° |
| argument of perigee: | 207.6192° |
| revolutions per day: | 14.74034002 |
| mean anomaly at epoch: | 152.1517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|