View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 49319U 21091E 24358.22929747 .00022920 00000-0 61214-3 0 9995
2 49319 97.4354 192.7330 0011610 125.8127 234.4199 15.38040448177554
| Epoch (UTC): | 23 December 2024 05:30:11 |
| Eccentricity: | 0.0011610 |
| inclination: | 97.4354° |
| perigee height: | 444 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 192.7330° |
| argument of perigee: | 125.8127° |
| revolutions per day: | 15.38040448 |
| mean anomaly at epoch: | 234.4199° |
| orbit number at epoch: | 17755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|