View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00022U 59009A 25339.23827290 .00018315 00000-0 69402-3 0 9994
2 00022 50.2599 335.6995 0085916 63.9709 297.0065 15.23491252770725
| Epoch (UTC): | 05 December 2025 05:43:06 |
| Eccentricity: | 0.0085916 |
| inclination: | 50.2599° |
| perigee height: | 436 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 335.6995° |
| argument of perigee: | 63.9709° |
| revolutions per day: | 15.23491252 |
| mean anomaly at epoch: | 297.0065° |
| orbit number at epoch: | 77072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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