View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60730U 26145.25318803 +.00000000 +00000-0 +16061-4 0 00005
2 60730 53.1593 98.5712 0000941 90.7718 269.3408 15.69717145 00
| Epoch (UTC): | 25 May 2026 06:04:35 |
| Eccentricity: | 0.0000941 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 98.5712° |
| argument of perigee: | 90.7718° |
| revolutions per day: | 15.69717145 |
| mean anomaly at epoch: | 269.3408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|