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 09013U 76067B 25198.01646736 -.00000077 00000-0 -72157-4 0 9999
2 09013 65.8644 35.0300 0714567 356.4153 3.1869 12.35401471210914
| Epoch (UTC): | 17 July 2025 00:23:42 |
| Eccentricity: | 0.0714567 |
| inclination: | 65.8644° |
| perigee height: | 961 km |
| apogee height: | 2091 km |
| right ascension of ascending node: | 35.0300° |
| argument of perigee: | 356.4153° |
| revolutions per day: | 12.35401471 |
| mean anomaly at epoch: | 3.1869° |
| orbit number at epoch: | 21091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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