View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 23087U 94023A 25339.10976866 .00000007 00000-0 28465-4 0 9999
2 23087 71.0550 12.9741 0008743 191.4504 168.6421 14.14351385631430
| Epoch (UTC): | 05 December 2025 02:38:04 |
| Eccentricity: | 0.0008743 |
| inclination: | 71.0550° |
| perigee height: | 838 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 12.9741° |
| argument of perigee: | 191.4504° |
| revolutions per day: | 14.14351385 |
| mean anomaly at epoch: | 168.6421° |
| orbit number at epoch: | 63143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|