View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67552U 26145.40222616 +.00000000 +00000-0 +50750-3 0 00009
2 67552 97.2858 32.5013 0001928 94.5103 265.6360 15.33463712 05
| Epoch (UTC): | 25 May 2026 09:39:12 |
| Eccentricity: | 0.0001928 |
| inclination: | 97.2858° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.5013° |
| argument of perigee: | 94.5103° |
| revolutions per day: | 15.33463712 |
| mean anomaly at epoch: | 265.6360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|