View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27607U 26145.43020300 +.00000000 +00000-0 +10978-3 0 00003
2 27607 64.5514 199.3924 0075599 266.6349 92.6107 14.82991152 04
| Epoch (UTC): | 25 May 2026 10:19:29 |
| Eccentricity: | 0.0075599 |
| inclination: | 64.5514° |
| perigee height: | 567 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 199.3924° |
| argument of perigee: | 266.6349° |
| revolutions per day: | 14.82991152 |
| mean anomaly at epoch: | 92.6107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|