View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68161U 26145.48654008 +.00000000 +00000-0 +45689-3 0 00003
2 68161 97.2874 167.0947 0001065 4.1408 355.9843 15.33416087 09
| Epoch (UTC): | 25 May 2026 11:40:37 |
| Eccentricity: | 0.0001065 |
| inclination: | 97.2874° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.0947° |
| argument of perigee: | 4.1408° |
| revolutions per day: | 15.33416087 |
| mean anomaly at epoch: | 355.9843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|