View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29092U 26129.62610117 +.00000000 +00000-0 +56874-4 0 00003
2 29092 97.7484 151.4720 0001535 88.1727 271.9666 14.87690053 00
| Epoch (UTC): | 09 May 2026 15:01:35 |
| Eccentricity: | 0.0001535 |
| inclination: | 97.7484° |
| perigee height: | 604 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 151.4720° |
| argument of perigee: | 88.1727° |
| revolutions per day: | 14.87690053 |
| mean anomaly at epoch: | 271.9666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|