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 36416U 10009D 25197.22050434 .00000322 00000-0 97117-4 0 9990
2 36416 63.3904 236.8818 0669318 1.0697 359.1597 13.72208551768654
| Epoch (UTC): | 16 July 2025 05:17:31 |
| Eccentricity: | 0.0669318 |
| inclination: | 63.3904° |
| perigee height: | 498 km |
| apogee height: | 1485 km |
| right ascension of ascending node: | 236.8818° |
| argument of perigee: | 1.0697° |
| revolutions per day: | 13.72208551 |
| mean anomaly at epoch: | 359.1597° |
| orbit number at epoch: | 76865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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