View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53576U 26145.49936833 +.00000000 +00000-0 +34572-3 0 00006
2 53576 53.2135 69.1063 0001196 95.9651 264.1477 15.08814844 08
| Epoch (UTC): | 25 May 2026 11:59:05 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.1063° |
| argument of perigee: | 95.9651° |
| revolutions per day: | 15.08814844 |
| mean anomaly at epoch: | 264.1477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|