View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54179U 26145.02829566 +.00000000 +00000-0 -10316-3 0 00000
2 54179 53.2128 21.3154 0001372 96.6258 263.4890 15.08844873 04
| Epoch (UTC): | 25 May 2026 00:40:44 |
| Eccentricity: | 0.0001372 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 21.3154° |
| argument of perigee: | 96.6258° |
| revolutions per day: | 15.08844873 |
| mean anomaly at epoch: | 263.4890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|