View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28538U 05004B 23300.77874080 0.00000100 00000-0 15634-3 0 00
2 28538 63.8253 198.7789 0191912 308.9485 51.0515 13.43221466 03
| Epoch (UTC): | 27 October 2023 18:41:23 |
| Eccentricity: | 0.0191912 |
| inclination: | 63.8253° |
| perigee height: | 954 km |
| apogee height: | 1241 km |
| right ascension of ascending node: | 198.7789° |
| argument of perigee: | 308.9485° |
| revolutions per day: | 13.43221466 |
| mean anomaly at epoch: | 51.0515° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|