View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28649U 26075.79641764 +.00000000 +00000-0 +14542-3 0 00005
2 28649 97.5408 103.0266 0002071 61.1748 298.9679 14.90791154 00
| Epoch (UTC): | 16 March 2026 19:06:50 |
| Eccentricity: | 0.0002071 |
| inclination: | 97.5408° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.0266° |
| argument of perigee: | 61.1748° |
| revolutions per day: | 14.90791154 |
| mean anomaly at epoch: | 298.9679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|