View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 21949U 92023A 23085.99448066 0.00000400 00000-0 15036-3 0 00
2 21949 85.0091 33.4882 0002680 30.0246 329.9752 14.31643205 05
| Epoch (UTC): | 26 March 2023 23:52:03 |
| Eccentricity: | 0.0002680 |
| inclination: | 85.0091° |
| perigee height: | 784 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 33.4882° |
| argument of perigee: | 30.0246° |
| revolutions per day: | 14.31643205 |
| mean anomaly at epoch: | 329.9752° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|