View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29495U 26151.51518111 +.00000000 +00000-0 +00000-0 0 00000
2 29495 2.9929 79.8555 0003950 347.3222 159.2881 1.00271535 09
| Epoch (UTC): | 31 May 2026 12:21:51 |
| Eccentricity: | 0.0003950 |
| inclination: | 2.9929° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 79.8555° |
| argument of perigee: | 347.3222° |
| revolutions per day: | 1.00271535 |
| mean anomaly at epoch: | 159.2881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|