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 61923U 24207M 25341.27793817 .00042664 00000-0 15497-2 0 9995
2 61923 42.9994 87.5522 0000553 19.9698 340.1175 15.27607510 60544
| Epoch (UTC): | 07 December 2025 06:40:13 |
| Eccentricity: | 0.0000553 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 87.5522° |
| argument of perigee: | 19.9698° |
| revolutions per day: | 15.27607510 |
| mean anomaly at epoch: | 340.1175° |
| orbit number at epoch: | 6054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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