View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00082U 61004B 23030.89470736 .00000215 00000-0 23027-3 0 9998
2 00082 38.8513 253.4388 1167333 24.0550 341.0444 12.26087525925322
| Epoch (UTC): | 30 January 2023 21:28:22 |
| Eccentricity: | 0.1167333 |
| inclination: | 38.8513° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 253.4388° |
| argument of perigee: | 24.0550° |
| revolutions per day: | 12.26087525 |
| mean anomaly at epoch: | 341.0444° |
| orbit number at epoch: | 92532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|