View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 37900U 99025EMZ 24351.12757045 .00011183 00000-0 62725-2 0 9998
2 37900 102.2957 296.7891 0225422 35.7367 325.8638 13.98812285774209
| Epoch (UTC): | 16 December 2024 03:03:42 |
| Eccentricity: | 0.0225422 |
| inclination: | 102.2957° |
| perigee height: | 734 km |
| apogee height: | 1062 km |
| right ascension of ascending node: | 296.7891° |
| argument of perigee: | 35.7367° |
| revolutions per day: | 13.98812285 |
| mean anomaly at epoch: | 325.8638° |
| orbit number at epoch: | 77420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|