View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 02801U 26087.70358529 +.00000000 +00000-0 +18370-4 0 00009
2 02801 74.0405 213.0124 0055826 80.2912 280.4541 14.36933215 05
| Epoch (UTC): | 28 March 2026 16:53:09 |
| Eccentricity: | 0.0055826 |
| inclination: | 74.0405° |
| perigee height: | 729 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 213.0124° |
| argument of perigee: | 80.2912° |
| revolutions per day: | 14.36933215 |
| mean anomaly at epoch: | 280.4541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|