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 00029U 60002B 25350.81407462 .00000581 00000-0 10758-3 0 9994
2 00029 48.3767 171.1670 0022674 204.1455 155.8397 14.78423931515149
| Epoch (UTC): | 16 December 2025 19:32:16 |
| Eccentricity: | 0.0022674 |
| inclination: | 48.3767° |
| perigee height: | 618 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 171.1670° |
| argument of perigee: | 204.1455° |
| revolutions per day: | 14.78423931 |
| mean anomaly at epoch: | 155.8397° |
| orbit number at epoch: | 51514 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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