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 25197.51126723 .00000010 00000-0 -10276-5 0 9990
2 07714 81.1971 197.1911 0029467 216.2991 143.6180 14.08420819900284
| Epoch (UTC): | 16 July 2025 12:16:13 |
| Eccentricity: | 0.0029467 |
| inclination: | 81.1971° |
| perigee height: | 843 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 197.1911° |
| argument of perigee: | 216.2991° |
| revolutions per day: | 14.08420819 |
| mean anomaly at epoch: | 143.6180° |
| orbit number at epoch: | 90028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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