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 25340.58690681 .00000206 00000-0 11270-3 0 9995
2 07714 81.1965 57.5728 0030589 175.0461 185.1018 14.08447703920423
| Epoch (UTC): | 06 December 2025 14:05:08 |
| Eccentricity: | 0.0030589 |
| inclination: | 81.1965° |
| perigee height: | 842 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 57.5728° |
| argument of perigee: | 175.0461° |
| revolutions per day: | 14.08447703 |
| mean anomaly at epoch: | 185.1018° |
| orbit number at epoch: | 92042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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