View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29048U 26053.54984241 +.00000000 +00000-0 +15168-3 0 00003
2 29048 71.9646 94.9059 0040878 36.2391 324.1502 14.31279585 07
| Epoch (UTC): | 22 February 2026 13:11:46 |
| Eccentricity: | 0.0040878 |
| inclination: | 71.9646° |
| perigee height: | 758 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 94.9059° |
| argument of perigee: | 36.2391° |
| revolutions per day: | 14.31279585 |
| mean anomaly at epoch: | 324.1502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|