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 27819U 03023B 25193.92913906 .00000116 00000-0 10499-3 0 9998
2 27819 82.9483 5.3012 0047533 127.3282 36.8457 13.74495688108626
| Epoch (UTC): | 12 July 2025 22:17:57 |
| Eccentricity: | 0.0047533 |
| inclination: | 82.9483° |
| perigee height: | 948 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 5.3012° |
| argument of perigee: | 127.3282° |
| revolutions per day: | 13.74495688 |
| mean anomaly at epoch: | 36.8457° |
| orbit number at epoch: | 10862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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