View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62401U 26145.42446601 +.00000000 +00000-0 +49209-3 0 00008
2 62401 44.9740 36.6441 0006180 153.9507 206.1692 15.38584650 03
| Epoch (UTC): | 25 May 2026 10:11:13 |
| Eccentricity: | 0.0006180 |
| inclination: | 44.9740° |
| perigee height: | 446 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 36.6441° |
| argument of perigee: | 153.9507° |
| revolutions per day: | 15.38584650 |
| mean anomaly at epoch: | 206.1692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|