View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67129U 26145.20101376 +.00000000 +00000-0 +58370-3 0 00002
2 67129 43.0018 97.2371 0001636 268.6006 91.4658 15.27591234 08
| Epoch (UTC): | 25 May 2026 04:49:27 |
| Eccentricity: | 0.0001636 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 97.2371° |
| argument of perigee: | 268.6006° |
| revolutions per day: | 15.27591234 |
| mean anomaly at epoch: | 91.4658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|