View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53859U 26145.17684645 +.00000000 +00000-0 +24872-4 0 00009
2 53859 53.2144 305.4110 0000832 70.6770 289.4312 15.08837564 01
| Epoch (UTC): | 25 May 2026 04:14:39 |
| Eccentricity: | 0.0000832 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 305.4110° |
| argument of perigee: | 70.6770° |
| revolutions per day: | 15.08837564 |
| mean anomaly at epoch: | 289.4312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|