View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 17296U 87003B 23150.49501686 .00000428 00000-0 48722-4 0 9994
2 17296 82.5277 151.9294 0017146 253.4960 106.4371 14.83844086944204
| Epoch (UTC): | 30 May 2023 11:52:49 |
| Eccentricity: | 0.0017146 |
| inclination: | 82.5277° |
| perigee height: | 605 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 151.9294° |
| argument of perigee: | 253.4960° |
| revolutions per day: | 14.83844086 |
| mean anomaly at epoch: | 106.4371° |
| orbit number at epoch: | 94420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|