View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52288U 26145.33788850 +.00000000 +00000-0 +65621-4 0 00002
2 52288 53.2133 115.0349 0001531 78.5362 281.5802 15.08847414 06
| Epoch (UTC): | 25 May 2026 08:06:33 |
| Eccentricity: | 0.0001531 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.0349° |
| argument of perigee: | 78.5362° |
| revolutions per day: | 15.08847414 |
| mean anomaly at epoch: | 281.5802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|