View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67317U 26144.98790273 +.00000000 +00000-0 +13175-2 0 00008
2 67317 43.0010 254.7323 0001624 291.1084 68.9594 15.27606358 02
| Epoch (UTC): | 24 May 2026 23:42:34 |
| Eccentricity: | 0.0001624 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.7323° |
| argument of perigee: | 291.1084° |
| revolutions per day: | 15.27606358 |
| mean anomaly at epoch: | 68.9594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|