View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28892U 26150.39015866 +.00000000 +00000-0 +28312-3 0 00003
2 28892 98.3050 306.2084 0012469 265.9969 93.9812 14.72065965 04
| Epoch (UTC): | 30 May 2026 09:21:49 |
| Eccentricity: | 0.0012469 |
| inclination: | 98.3050° |
| perigee height: | 646 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 306.2084° |
| argument of perigee: | 265.9969° |
| revolutions per day: | 14.72065965 |
| mean anomaly at epoch: | 93.9812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|