View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60916U 26145.09965383 +.00000000 +00000-0 -37079-4 0 00007
2 60916 53.1608 288.9256 0000939 100.3355 259.7752 15.30203921 08
| Epoch (UTC): | 25 May 2026 02:23:30 |
| Eccentricity: | 0.0000939 |
| inclination: | 53.1608° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.9256° |
| argument of perigee: | 100.3355° |
| revolutions per day: | 15.30203921 |
| mean anomaly at epoch: | 259.7752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|