View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53531U 26145.14332705 +.00000000 +00000-0 -73923-4 0 00002
2 53531 53.2124 90.9067 0001545 81.1835 278.9332 15.08822095 02
| Epoch (UTC): | 25 May 2026 03:26:23 |
| Eccentricity: | 0.0001545 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 90.9067° |
| argument of perigee: | 81.1835° |
| revolutions per day: | 15.08822095 |
| mean anomaly at epoch: | 278.9332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|