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 10513U 77116B 25188.61902259 -.00000089 00000-0 -74458-5 0 9992
2 10513 65.8321 12.8726 0024147 2.1596 58.4736 13.78824439393326
| Epoch (UTC): | 07 July 2025 14:51:23 |
| Eccentricity: | 0.0024147 |
| inclination: | 65.8321° |
| perigee height: | 950 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 12.8726° |
| argument of perigee: | 2.1596° |
| revolutions per day: | 13.78824439 |
| mean anomaly at epoch: | 58.4736° |
| orbit number at epoch: | 39332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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