View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29228U 26050.81350064 +.00000000 +00000-0 +11682-3 0 00007
2 29228 69.9320 283.2644 0003281 184.7236 175.3900 15.12631902 03
| Epoch (UTC): | 19 February 2026 19:31:26 |
| Eccentricity: | 0.0003281 |
| inclination: | 69.9320° |
| perigee height: | 526 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 283.2644° |
| argument of perigee: | 184.7236° |
| revolutions per day: | 15.12631902 |
| mean anomaly at epoch: | 175.3900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|