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 19070U 88033A 25163.55296299 .00000069 00000-0 12532-3 0 9994
2 19070 90.3164 10.6911 0188559 330.4657 80.8135 13.27756069798492
| Epoch (UTC): | 12 June 2025 13:16:16 |
| Eccentricity: | 0.0188559 |
| inclination: | 90.3164° |
| perigee height: | 1013 km |
| apogee height: | 1297 km |
| right ascension of ascending node: | 10.6911° |
| argument of perigee: | 330.4657° |
| revolutions per day: | 13.27756069 |
| mean anomaly at epoch: | 80.8135° |
| orbit number at epoch: | 79849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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