View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62675U 26144.73243992 +.00000000 +00000-0 +31057-3 0 00004
2 62675 97.4014 226.5907 0005615 59.6157 300.5637 15.28805565 03
| Epoch (UTC): | 24 May 2026 17:34:42 |
| Eccentricity: | 0.0005615 |
| inclination: | 97.4014° |
| perigee height: | 476 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 226.5907° |
| argument of perigee: | 59.6157° |
| revolutions per day: | 15.28805565 |
| mean anomaly at epoch: | 300.5637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|