View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62421U 26145.14217683 +.00000000 +00000-0 +20571-2 0 00005
2 62421 43.0014 66.9117 0003458 265.2370 94.8103 15.70973101 03
| Epoch (UTC): | 25 May 2026 03:24:44 |
| Eccentricity: | 0.0003458 |
| inclination: | 43.0014° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 66.9117° |
| argument of perigee: | 265.2370° |
| revolutions per day: | 15.70973101 |
| mean anomaly at epoch: | 94.8103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|