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 18958U 88020A 25191.26649567 .00001999 00000-0 10399-3 0 9995
2 18958 82.5149 130.2605 0003551 350.5248 9.5917 15.15499939 13482
| Epoch (UTC): | 10 July 2025 06:23:45 |
| Eccentricity: | 0.0003551 |
| inclination: | 82.5149° |
| perigee height: | 517 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 130.2605° |
| argument of perigee: | 350.5248° |
| revolutions per day: | 15.15499939 |
| mean anomaly at epoch: | 9.5917° |
| orbit number at epoch: | 1348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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