View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44881U 26069.96476888 +.00000000 +00000-0 +18283-3 0 00002
2 44881 97.7604 144.5722 0014837 53.9842 306.2747 14.86345925 05
| Epoch (UTC): | 10 March 2026 23:09:16 |
| Eccentricity: | 0.0014837 |
| inclination: | 97.7604° |
| perigee height: | 599 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 144.5722° |
| argument of perigee: | 53.9842° |
| revolutions per day: | 14.86345925 |
| mean anomaly at epoch: | 306.2747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|