View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41599U 26106.93862315 +.00000000 +00000-0 +84825-4 0 00004
2 41599 97.4545 167.7396 0009387 355.3274 4.7871 15.19176821 07
| Epoch (UTC): | 16 April 2026 22:31:37 |
| Eccentricity: | 0.0009387 |
| inclination: | 97.4545° |
| perigee height: | 502 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 167.7396° |
| argument of perigee: | 355.3274° |
| revolutions per day: | 15.19176821 |
| mean anomaly at epoch: | 4.7871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|