View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53610U 26144.66955855 +.00000000 +00000-0 +42016-4 0 00001
2 53610 53.2145 253.1564 0001038 95.5647 264.5463 15.08834332 08
| Epoch (UTC): | 24 May 2026 16:04:09 |
| Eccentricity: | 0.0001038 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 253.1564° |
| argument of perigee: | 95.5647° |
| revolutions per day: | 15.08834332 |
| mean anomaly at epoch: | 264.5463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|