View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40045U 26106.42589716 +.00000000 +00000-0 +30905-3 0 00003
2 40045 97.7189 274.0823 0038034 220.4771 139.3620 14.97387967 08
| Epoch (UTC): | 16 April 2026 10:13:17 |
| Eccentricity: | 0.0038034 |
| inclination: | 97.7189° |
| perigee height: | 549 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 274.0823° |
| argument of perigee: | 220.4771° |
| revolutions per day: | 14.97387967 |
| mean anomaly at epoch: | 139.3620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|