View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63400U 26145.38036065 +.00000000 +00000-0 +79976-3 0 00006
2 63400 43.0008 33.5521 0001544 266.9352 93.1323 15.27564267 02
| Epoch (UTC): | 25 May 2026 09:07:43 |
| Eccentricity: | 0.0001544 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.5521° |
| argument of perigee: | 266.9352° |
| revolutions per day: | 15.27564267 |
| mean anomaly at epoch: | 93.1323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|