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 23029.91683728 .00000225 00000-0 23747-3 0 9996
2 00082 38.8516 257.0594 1167362 19.3349 344.8076 12.26087000925206
| Epoch (UTC): | 29 January 2023 22:00:14 |
| Eccentricity: | 0.1167362 |
| inclination: | 38.8516° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 257.0594° |
| argument of perigee: | 19.3349° |
| revolutions per day: | 12.26087000 |
| mean anomaly at epoch: | 344.8076° |
| orbit number at epoch: | 92520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|