View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62213U 26145.42550079 +.00000000 +00000-0 +73393-3 0 00005
2 62213 43.0011 197.6442 0002720 278.5357 81.5187 15.27565589 09
| Epoch (UTC): | 25 May 2026 10:12:43 |
| Eccentricity: | 0.0002720 |
| inclination: | 43.0011° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 197.6442° |
| argument of perigee: | 278.5357° |
| revolutions per day: | 15.27565589 |
| mean anomaly at epoch: | 81.5187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|