View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40420U 26145.41642503 +.00000000 +00000-0 +86986-4 0 00007
2 40420 97.8322 201.7527 0015358 334.2376 25.8084 15.06522202 09
| Epoch (UTC): | 25 May 2026 09:59:39 |
| Eccentricity: | 0.0015358 |
| inclination: | 97.8322° |
| perigee height: | 536 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 201.7527° |
| argument of perigee: | 334.2376° |
| revolutions per day: | 15.06522202 |
| mean anomaly at epoch: | 25.8084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|