View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27059U 01058E 23084.16461057 .00000053 00000-0 24171-3 0 9990
2 27059 82.5376 248.3487 0002385 54.9449 305.1863 12.61510663978017
| Epoch (UTC): | 25 March 2023 03:57:02 |
| Eccentricity: | 0.0002385 |
| inclination: | 82.5376° |
| perigee height: | 1415 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 248.3487° |
| argument of perigee: | 54.9449° |
| revolutions per day: | 12.61510663 |
| mean anomaly at epoch: | 305.1863° |
| orbit number at epoch: | 97801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|