View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65199U 26145.43630409 +.00000000 +00000-0 +87365-3 0 00002
2 65199 53.1595 155.3352 0001293 90.1951 269.9200 15.34388827 01
| Epoch (UTC): | 25 May 2026 10:28:16 |
| Eccentricity: | 0.0001293 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.3352° |
| argument of perigee: | 90.1951° |
| revolutions per day: | 15.34388827 |
| mean anomaly at epoch: | 269.9200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|