View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62027U 26145.47273678 +.00000000 +00000-0 +83662-3 0 00000
2 62027 53.1586 171.2630 0001172 77.7954 282.3178 15.30200050 04
| Epoch (UTC): | 25 May 2026 11:20:44 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.2630° |
| argument of perigee: | 77.7954° |
| revolutions per day: | 15.30200050 |
| mean anomaly at epoch: | 282.3178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|