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 23276.53340670 .00000288 00000-0 10815-3 0 9991
2 27386 98.2446 242.1549 0001239 88.3139 24.3571 14.38416760131530
| Epoch (UTC): | 03 October 2023 12:48:06 |
| Eccentricity: | 0.0001239 |
| inclination: | 98.2446° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 242.1549° |
| argument of perigee: | 88.3139° |
| revolutions per day: | 14.38416760 |
| mean anomaly at epoch: | 24.3571° |
| orbit number at epoch: | 13153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|