View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68144U 26145.06510131 +.00000000 +00000-0 +44001-3 0 00003
2 68144 97.2844 166.7480 0000768 107.2100 252.9227 15.33457305 08
| Epoch (UTC): | 25 May 2026 01:33:44 |
| Eccentricity: | 0.0000768 |
| inclination: | 97.2844° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.7480° |
| argument of perigee: | 107.2100° |
| revolutions per day: | 15.33457305 |
| mean anomaly at epoch: | 252.9227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|