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 43445U 18036E 25108.56747568 .00000058 00000-0 00000+0 0 9994
2 43445 6.0801 71.9994 0010222 154.3660 354.7403 1.02111630 22586
| Epoch (UTC): | 18 April 2025 13:37:09 |
| Eccentricity: | 0.0010222 |
| inclination: | 6.0801° |
| perigee height: | 35235 km |
| apogee height: | 35321 km |
| right ascension of ascending node: | 71.9994° |
| argument of perigee: | 154.3660° |
| revolutions per day: | 1.02111630 |
| mean anomaly at epoch: | 354.7403° |
| orbit number at epoch: | 2258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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