View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40286U 26145.59699514 +.00000000 +00000-0 +13238-3 0 00009
2 40286 98.3489 290.0682 0011034 306.7484 53.2705 14.66141233 04
| Epoch (UTC): | 25 May 2026 14:19:40 |
| Eccentricity: | 0.0011034 |
| inclination: | 98.3489° |
| perigee height: | 666 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 290.0682° |
| argument of perigee: | 306.7484° |
| revolutions per day: | 14.66141233 |
| mean anomaly at epoch: | 53.2705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|