View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68003U 26144.88130727 +.00000000 +00000-0 +64811-3 0 00006
2 68003 43.0012 338.8397 0001444 272.6036 87.4650 15.27594253 02
| Epoch (UTC): | 24 May 2026 21:09:04 |
| Eccentricity: | 0.0001444 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.8397° |
| argument of perigee: | 272.6036° |
| revolutions per day: | 15.27594253 |
| mean anomaly at epoch: | 87.4650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|