View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53598U 26145.03195816 +.00000000 +00000-0 +14636-5 0 00009
2 53598 53.2141 261.1445 0001310 90.3170 269.7972 15.08831266 08
| Epoch (UTC): | 25 May 2026 00:46:01 |
| Eccentricity: | 0.0001310 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 261.1445° |
| argument of perigee: | 90.3170° |
| revolutions per day: | 15.08831266 |
| mean anomaly at epoch: | 269.7972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|