View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47234U 26058.13989985 +.00000000 +00000-0 +17329-3 0 00001
2 47234 28.9961 20.3521 0010700 243.6219 116.3280 15.00334340 09
| Epoch (UTC): | 27 February 2026 03:21:27 |
| Eccentricity: | 0.0010700 |
| inclination: | 28.9961° |
| perigee height: | 558 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 20.3521° |
| argument of perigee: | 243.6219° |
| revolutions per day: | 15.00334340 |
| mean anomaly at epoch: | 116.3280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|