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 07714U 75023A 25136.41603132 .00000063 00000-0 29192-4 0 9999
2 07714 81.2000 256.7915 0027962 34.7397 325.5591 14.08417144891682
| Epoch (UTC): | 16 May 2025 09:59:05 |
| Eccentricity: | 0.0027962 |
| inclination: | 81.2000° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 256.7915° |
| argument of perigee: | 34.7397° |
| revolutions per day: | 14.08417144 |
| mean anomaly at epoch: | 325.5591° |
| orbit number at epoch: | 89168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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