View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62126U 26145.45883021 +.00000000 +00000-0 +13378-2 0 00003
2 62126 42.9989 62.3031 0001155 256.4812 103.5911 15.27607109 03
| Epoch (UTC): | 25 May 2026 11:00:42 |
| Eccentricity: | 0.0001155 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.3031° |
| argument of perigee: | 256.4812° |
| revolutions per day: | 15.27607109 |
| mean anomaly at epoch: | 103.5911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|