View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52991U 26145.31351436 +.00000000 +00000-0 +55591-4 0 00002
2 52991 53.2129 120.1440 0000985 83.2463 276.8641 15.08836597 06
| Epoch (UTC): | 25 May 2026 07:31:27 |
| Eccentricity: | 0.0000985 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 120.1440° |
| argument of perigee: | 83.2463° |
| revolutions per day: | 15.08836597 |
| mean anomaly at epoch: | 276.8641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|