View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27386U 02009A 25140.61541874 .00000118 00000-0 52198-4 0 9994
2 27386 98.3323 96.9678 0001247 91.1424 82.3804 14.38912714217023
| Epoch (UTC): | 20 May 2025 14:46:12 |
| Eccentricity: | 0.0001247 |
| inclination: | 98.3323° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 96.9678° |
| argument of perigee: | 91.1424° |
| revolutions per day: | 14.38912714 |
| mean anomaly at epoch: | 82.3804° |
| orbit number at epoch: | 21702 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|