View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67577U 26145.61124685 +.00000000 +00000-0 +63168-3 0 00003
2 67577 97.2868 205.9513 0000599 229.4327 130.6864 15.33448506 08
| Epoch (UTC): | 25 May 2026 14:40:11 |
| Eccentricity: | 0.0000599 |
| inclination: | 97.2868° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9513° |
| argument of perigee: | 229.4327° |
| revolutions per day: | 15.33448506 |
| mean anomaly at epoch: | 130.6864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|