View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62627U 26145.31897384 +.00000000 +00000-0 +13140-3 0 00009
2 62627 97.3989 224.0600 0008663 7.3814 352.7548 15.20577367 07
| Epoch (UTC): | 25 May 2026 07:39:19 |
| Eccentricity: | 0.0008663 |
| inclination: | 97.3989° |
| perigee height: | 498 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 224.0600° |
| argument of perigee: | 7.3814° |
| revolutions per day: | 15.20577367 |
| mean anomaly at epoch: | 352.7548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|