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 7493U 74083B 25197.34752762 .00000255 00000-0 13808-3 0 9990
2 7493 81.1606 152.8839 0085565 64.3185 296.6789 14.07960831604005
| Epoch (UTC): | 16 July 2025 08:20:26 |
| Eccentricity: | 0.0085565 |
| inclination: | 81.1606° |
| perigee height: | 804 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 152.8839° |
| argument of perigee: | 64.3185° |
| revolutions per day: | 14.07960831 |
| mean anomaly at epoch: | 296.6789° |
| orbit number at epoch: | 60400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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