View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41579U 26150.60018470 +.00000000 +00000-0 +43012-4 0 00003
2 41579 99.1880 159.7192 0001094 86.1278 274.0003 13.85908808 09
| Epoch (UTC): | 30 May 2026 14:24:15 |
| Eccentricity: | 0.0001094 |
| inclination: | 99.1880° |
| perigee height: | 942 km |
| apogee height: | 944 km |
| right ascension of ascending node: | 159.7192° |
| argument of perigee: | 86.1278° |
| revolutions per day: | 13.85908808 |
| mean anomaly at epoch: | 274.0003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|