View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62672U 26145.49402800 +.00000000 +00000-0 +17665-3 0 00009
2 62672 97.3953 224.9409 0005993 65.5012 294.6849 15.22739433 07
| Epoch (UTC): | 25 May 2026 11:51:24 |
| Eccentricity: | 0.0005993 |
| inclination: | 97.3953° |
| perigee height: | 493 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 224.9409° |
| argument of perigee: | 65.5012° |
| revolutions per day: | 15.22739433 |
| mean anomaly at epoch: | 294.6849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|