View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51127U 26145.46028764 +.00000000 +00000-0 -14558-4 0 00002
2 51127 53.2132 314.4939 0001263 87.6857 272.4280 15.08839913 02
| Epoch (UTC): | 25 May 2026 11:02:48 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.4939° |
| argument of perigee: | 87.6857° |
| revolutions per day: | 15.08839913 |
| mean anomaly at epoch: | 272.4280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|