View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51731U 26145.51636990 +.00000000 +00000-0 +33580-4 0 00000
2 51731 53.2130 334.2309 0001331 87.2830 272.8315 15.08837723 05
| Epoch (UTC): | 25 May 2026 12:23:34 |
| Eccentricity: | 0.0001331 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.2309° |
| argument of perigee: | 87.2830° |
| revolutions per day: | 15.08837723 |
| mean anomaly at epoch: | 272.8315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|