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 14148U 83061B 25199.74959546 .00000325 00000-0 34920-4 0 9993
2 14148 82.5174 21.2420 0019703 314.0632 45.8961 14.85361339251663
| Epoch (UTC): | 18 July 2025 17:59:25 |
| Eccentricity: | 0.0019703 |
| inclination: | 82.5174° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 21.2420° |
| argument of perigee: | 314.0632° |
| revolutions per day: | 14.85361339 |
| mean anomaly at epoch: | 45.8961° |
| orbit number at epoch: | 25166 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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