View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62434U 26145.57278416 +.00000000 +00000-0 +51006-3 0 00005
2 62434 53.1595 337.9040 0001170 88.6290 271.4845 15.30192991 08
| Epoch (UTC): | 25 May 2026 13:44:48 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 337.9040° |
| argument of perigee: | 88.6290° |
| revolutions per day: | 15.30192991 |
| mean anomaly at epoch: | 271.4845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|