View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67158U 26145.23245057 +.00000000 +00000-0 -92764-5 0 00000
2 67158 51.9042 92.1880 0000836 97.2937 262.8121 14.79935481 05
| Epoch (UTC): | 25 May 2026 05:34:43 |
| Eccentricity: | 0.0000836 |
| inclination: | 51.9042° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 92.1880° |
| argument of perigee: | 97.2937° |
| revolutions per day: | 14.79935481 |
| mean anomaly at epoch: | 262.8121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|