View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68160U 26145.02430421 +.00000000 +00000-0 +58342-3 0 00003
2 68160 97.2858 166.6509 0000839 56.9503 303.1820 15.33444690 09
| Epoch (UTC): | 25 May 2026 00:34:59 |
| Eccentricity: | 0.0000839 |
| inclination: | 97.2858° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.6509° |
| argument of perigee: | 56.9503° |
| revolutions per day: | 15.33444690 |
| mean anomaly at epoch: | 303.1820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|