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 25341.29394733 .00000285 00000-0 10627-3 0 9996
2 27386 98.3592 292.1728 0001150 81.8549 86.0595 14.38996192245889
| Epoch (UTC): | 07 December 2025 07:03:17 |
| Eccentricity: | 0.0001150 |
| inclination: | 98.3592° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 292.1728° |
| argument of perigee: | 81.8549° |
| revolutions per day: | 14.38996192 |
| mean anomaly at epoch: | 86.0595° |
| orbit number at epoch: | 24588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|