View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28931U 26150.39321453 +.00000000 +00000-0 +24799-3 0 00004
2 28931 98.1316 106.0177 0002021 69.4680 290.6742 14.70009582 09
| Epoch (UTC): | 30 May 2026 09:26:13 |
| Eccentricity: | 0.0002021 |
| inclination: | 98.1316° |
| perigee height: | 660 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 106.0177° |
| argument of perigee: | 69.4680° |
| revolutions per day: | 14.70009582 |
| mean anomaly at epoch: | 290.6742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|