View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67070U 26145.54644053 +.00000000 +00000-0 +21938-3 0 00008
2 67070 41.3594 246.8248 0016245 63.0319 297.2160 15.17452396 02
| Epoch (UTC): | 25 May 2026 13:06:52 |
| Eccentricity: | 0.0016245 |
| inclination: | 41.3594° |
| perigee height: | 502 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 246.8248° |
| argument of perigee: | 63.0319° |
| revolutions per day: | 15.17452396 |
| mean anomaly at epoch: | 297.2160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|