View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27464U 26145.61437801 +.00000000 +00000-0 -10622-3 0 00009
2 27464 82.4860 359.0728 0024926 309.8386 50.0502 12.44622050 05
| Epoch (UTC): | 25 May 2026 14:44:42 |
| Eccentricity: | 0.0024926 |
| inclination: | 82.4860° |
| perigee height: | 1467 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 359.0728° |
| argument of perigee: | 309.8386° |
| revolutions per day: | 12.44622050 |
| mean anomaly at epoch: | 50.0502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|