View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39420U 13066E 23088.70888585 .00003258 00000-0 54951-3 0 9999
2 39420 97.8169 357.4529 0133056 171.8271 188.5144 14.64408246498999
| Epoch (UTC): | 29 March 2023 17:00:47 |
| Eccentricity: | 0.0133056 |
| inclination: | 97.8169° |
| perigee height: | 585 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 357.4529° |
| argument of perigee: | 171.8271° |
| revolutions per day: | 14.64408246 |
| mean anomaly at epoch: | 188.5144° |
| orbit number at epoch: | 49899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|