View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28895U 05043F 22176.85512726 .00000652 00000-0 13221-3 0 9993
2 28895 98.1077 308.1042 0017939 113.6657 246.6431 14.64360274888874
| Epoch (UTC): | 25 June 2022 20:31:22 |
| Eccentricity: | 0.0017939 |
| inclination: | 98.1077° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 308.1042° |
| argument of perigee: | 113.6657° |
| revolutions per day: | 14.64360274 |
| mean anomaly at epoch: | 246.6431° |
| orbit number at epoch: | 88887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|