View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63281U 26145.41616829 +.00000000 +00000-0 +59990-3 0 00003
2 63281 43.0020 167.9527 0001506 270.8547 89.2132 15.27599293 00
| Epoch (UTC): | 25 May 2026 09:59:16 |
| Eccentricity: | 0.0001506 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.9527° |
| argument of perigee: | 270.8547° |
| revolutions per day: | 15.27599293 |
| mean anomaly at epoch: | 89.2132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|