View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59448U 26145.14315512 +.00000000 +00000-0 +12382-3 0 00002
2 59448 45.6037 35.4595 0003585 263.8906 96.1567 14.99055161 08
| Epoch (UTC): | 25 May 2026 03:26:08 |
| Eccentricity: | 0.0003585 |
| inclination: | 45.6037° |
| perigee height: | 567 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 35.4595° |
| argument of perigee: | 263.8906° |
| revolutions per day: | 14.99055161 |
| mean anomaly at epoch: | 96.1567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|