View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60083U 26145.32918838 +.00000000 +00000-0 -80285-5 0 00009
2 60083 97.8953 169.1023 0001150 297.7133 62.3963 14.80581459 05
| Epoch (UTC): | 25 May 2026 07:54:01 |
| Eccentricity: | 0.0001150 |
| inclination: | 97.8953° |
| perigee height: | 627 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 169.1023° |
| argument of perigee: | 297.7133° |
| revolutions per day: | 14.80581459 |
| mean anomaly at epoch: | 62.3963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|