View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28932U 06002B 25196.89484168 .00004252 00000-0 24750-3 0 9997
2 28932 98.2155 320.0405 0057372 325.3713 34.3784 15.11274763 58614
| Epoch (UTC): | 15 July 2025 21:28:34 |
| Eccentricity: | 0.0057372 |
| inclination: | 98.2155° |
| perigee height: | 492 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 320.0405° |
| argument of perigee: | 325.3713° |
| revolutions per day: | 15.11274763 |
| mean anomaly at epoch: | 34.3784° |
| orbit number at epoch: | 5861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|