View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68152U 26145.50555862 +.00000000 +00000-0 +42012-3 0 00001
2 68152 97.2844 167.2194 0000796 132.5317 227.5993 15.33452789 06
| Epoch (UTC): | 25 May 2026 12:08:00 |
| Eccentricity: | 0.0000796 |
| inclination: | 97.2844° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.2194° |
| argument of perigee: | 132.5317° |
| revolutions per day: | 15.33452789 |
| mean anomaly at epoch: | 227.5993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|