View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62147U 26144.97286356 +.00000000 +00000-0 +81683-3 0 00005
2 62147 42.9995 87.5424 0001567 269.7067 90.3605 15.27591268 05
| Epoch (UTC): | 24 May 2026 23:20:55 |
| Eccentricity: | 0.0001567 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.5424° |
| argument of perigee: | 269.7067° |
| revolutions per day: | 15.27591268 |
| mean anomaly at epoch: | 90.3605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|