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 28419U 04037A 25133.91299018 .00000029 00000-0 12935-3 0 9995
2 28419 82.4866 215.9695 0016895 66.9691 293.3170 12.45668315938199
| Epoch (UTC): | 13 May 2025 21:54:42 |
| Eccentricity: | 0.0016895 |
| inclination: | 82.4866° |
| perigee height: | 1469 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 215.9695° |
| argument of perigee: | 66.9691° |
| revolutions per day: | 12.45668315 |
| mean anomaly at epoch: | 293.3170° |
| orbit number at epoch: | 93819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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