View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65450U 26145.31772940 +.00000000 +00000-0 +30945-3 0 00008
2 65450 97.4481 359.4724 0002343 74.7341 285.4145 15.05645827 09
| Epoch (UTC): | 25 May 2026 07:37:31 |
| Eccentricity: | 0.0002343 |
| inclination: | 97.4481° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.4724° |
| argument of perigee: | 74.7341° |
| revolutions per day: | 15.05645827 |
| mean anomaly at epoch: | 285.4145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|