View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 15427U 84123A 25131.80081632 .00000160 00000-0 10271-3 0 9998
2 15427 99.1226 143.5361 0015464 49.5173 123.1843 14.16915240 86573
| Epoch (UTC): | 11 May 2025 19:13:10 |
| Eccentricity: | 0.0015464 |
| inclination: | 99.1226° |
| perigee height: | 824 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 143.5361° |
| argument of perigee: | 49.5173° |
| revolutions per day: | 14.16915240 |
| mean anomaly at epoch: | 123.1843° |
| orbit number at epoch: | 8657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|