View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28738U 26020.98876480 +.00000000 +00000-0 +68653-3 0 00002
2 28738 97.3617 34.5385 0005146 168.3480 191.7895 15.55934407 00
| Epoch (UTC): | 20 January 2026 23:43:49 |
| Eccentricity: | 0.0005146 |
| inclination: | 97.3617° |
| perigee height: | 396 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 34.5385° |
| argument of perigee: | 168.3480° |
| revolutions per day: | 15.55934407 |
| mean anomaly at epoch: | 191.7895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|