View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54177U 26145.03199403 +.00000000 +00000-0 -14169-3 0 00009
2 54177 53.2141 21.3375 0001379 91.1667 268.9483 15.08829443 07
| Epoch (UTC): | 25 May 2026 00:46:04 |
| Eccentricity: | 0.0001379 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 21.3375° |
| argument of perigee: | 91.1667° |
| revolutions per day: | 15.08829443 |
| mean anomaly at epoch: | 268.9483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|