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 09904U 77024B 25194.60559805 -.00000066 00000-0 -45864-4 0 9996
2 09904 81.2639 160.4179 0052089 303.2133 56.4048 14.07264669477167
| Epoch (UTC): | 13 July 2025 14:32:03 |
| Eccentricity: | 0.0052089 |
| inclination: | 81.2639° |
| perigee height: | 831 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 160.4179° |
| argument of perigee: | 303.2133° |
| revolutions per day: | 14.07264669 |
| mean anomaly at epoch: | 56.4048° |
| orbit number at epoch: | 47716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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