View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59306U 26145.50475205 +.00000000 +00000-0 +23413-4 0 00009
2 59306 43.0014 156.7716 0001236 268.8586 91.2124 15.27576528 02
| Epoch (UTC): | 25 May 2026 12:06:50 |
| Eccentricity: | 0.0001236 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 156.7716° |
| argument of perigee: | 268.8586° |
| revolutions per day: | 15.27576528 |
| mean anomaly at epoch: | 91.2124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|