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 65719U 25214H 25341.29639528 .00005681 00000-0 65165-3 0 9997
2 65719 49.9793 117.2354 0012818 229.4002 130.5823 14.87030324 11032
| Epoch (UTC): | 07 December 2025 07:06:48 |
| Eccentricity: | 0.0012818 |
| inclination: | 49.9793° |
| perigee height: | 598 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 117.2354° |
| argument of perigee: | 229.4002° |
| revolutions per day: | 14.87030324 |
| mean anomaly at epoch: | 130.5823° |
| orbit number at epoch: | 1103 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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