View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00016U 58002A 25316.74694548 .00000103 00000-0 11813-3 0 9997
2 00016 34.2757 210.9624 2024480 286.5402 52.3295 10.49569897666178
| Epoch (UTC): | 12 November 2025 17:55:36 |
| Eccentricity: | 0.2024480 |
| inclination: | 34.2757° |
| perigee height: | 649 km |
| apogee height: | 4217 km |
| right ascension of ascending node: | 210.9624° |
| argument of perigee: | 286.5402° |
| revolutions per day: | 10.49569897 |
| mean anomaly at epoch: | 52.3295° |
| orbit number at epoch: | 66617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|