View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59652U 26145.18287648 +.00000000 +00000-0 +28040-4 0 00000
2 59652 43.0020 57.1438 0000811 269.5644 90.5114 15.27584545 08
| Epoch (UTC): | 25 May 2026 04:23:20 |
| Eccentricity: | 0.0000811 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 57.1438° |
| argument of perigee: | 269.5644° |
| revolutions per day: | 15.27584545 |
| mean anomaly at epoch: | 90.5114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|