View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00107U 61013A 25345.21379251 .00002472 00000-0 28467-3 0 9993
2 00107 28.7832 319.4711 0498618 173.8931 186.8006 14.21007208249722
| Epoch (UTC): | 11 December 2025 05:07:51 |
| Eccentricity: | 0.0498618 |
| inclination: | 28.7832° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 319.4711° |
| argument of perigee: | 173.8931° |
| revolutions per day: | 14.21007208 |
| mean anomaly at epoch: | 186.8006° |
| orbit number at epoch: | 24972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|