View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52771U 26145.42636419 +.00000000 +00000-0 +16189-3 0 00006
2 52771 97.4725 209.3140 0007761 49.8208 310.3684 14.81298023 02
| Epoch (UTC): | 25 May 2026 10:13:57 |
| Eccentricity: | 0.0007761 |
| inclination: | 97.4725° |
| perigee height: | 620 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 209.3140° |
| argument of perigee: | 49.8208° |
| revolutions per day: | 14.81298023 |
| mean anomaly at epoch: | 310.3684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|