View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53763U 26145.42723587 +.00000000 +00000-0 +23479-3 0 00001
2 53763 34.9898 140.2164 0001830 47.9422 312.1448 15.23154489 00
| Epoch (UTC): | 25 May 2026 10:15:13 |
| Eccentricity: | 0.0001830 |
| inclination: | 34.9898° |
| perigee height: | 495 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 140.2164° |
| argument of perigee: | 47.9422° |
| revolutions per day: | 15.23154489 |
| mean anomaly at epoch: | 312.1448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|