View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53273U 26145.33558959 +.00000000 +00000-0 +26295-3 0 00005
2 53273 53.2139 200.0446 0001283 97.3918 262.7220 15.08820926 04
| Epoch (UTC): | 25 May 2026 08:03:14 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 200.0446° |
| argument of perigee: | 97.3918° |
| revolutions per day: | 15.08820926 |
| mean anomaly at epoch: | 262.7220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|