View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00016U 26102.49914954 +.00000000 +00000-0 +86543-4 0 00006
2 00016 34.2631 134.9732 2019039 203.1715 146.3587 10.49583754 00
| Epoch (UTC): | 12 April 2026 11:58:46 |
| Eccentricity: | 0.2019039 |
| inclination: | 34.2631° |
| perigee height: | 654 km |
| apogee height: | 4213 km |
| right ascension of ascending node: | 134.9732° |
| argument of perigee: | 203.1715° |
| revolutions per day: | 10.49583754 |
| mean anomaly at epoch: | 146.3587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|