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 36519U 10017A 25197.93173512 .00000052 00000-0 41551-4 0 9995
2 36519 82.9621 136.0561 0035821 342.7465 82.8514 13.71633250761975
| Epoch (UTC): | 16 July 2025 22:21:41 |
| Eccentricity: | 0.0035821 |
| inclination: | 82.9621° |
| perigee height: | 967 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 136.0561° |
| argument of perigee: | 342.7465° |
| revolutions per day: | 13.71633250 |
| mean anomaly at epoch: | 82.8514° |
| orbit number at epoch: | 76197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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