View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46784U 26145.58335647 +.00000000 +00000-0 +76787-3 0 00009
2 46784 53.0458 254.2960 0005947 343.6400 150.2763 15.79305316 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005947 |
| inclination: | 53.0458° |
| perigee height: | 328 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 254.2960° |
| argument of perigee: | 343.6400° |
| revolutions per day: | 15.79305316 |
| mean anomaly at epoch: | 150.2763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|