View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 03598U 68110B 22145.38708872 .00000479 00000-0 11364-3 0 9996
2 03598 34.9925 232.4975 0048528 97.9205 262.7000 14.54684450808240
| Epoch (UTC): | 25 May 2022 09:17:24 |
| Eccentricity: | 0.0048528 |
| inclination: | 34.9925° |
| perigee height: | 676 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 232.4975° |
| argument of perigee: | 97.9205° |
| revolutions per day: | 14.54684450 |
| mean anomaly at epoch: | 262.7000° |
| orbit number at epoch: | 80824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|