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 28230U 04014A 25191.58221275 .00000476 00000-0 57231-4 0 9993
2 28230 89.8364 56.9276 0003474 86.2904 273.8718 14.82512185601726
| Epoch (UTC): | 10 July 2025 13:58:23 |
| Eccentricity: | 0.0003474 |
| inclination: | 89.8364° |
| perigee height: | 619 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 56.9276° |
| argument of perigee: | 86.2904° |
| revolutions per day: | 14.82512185 |
| mean anomaly at epoch: | 273.8718° |
| orbit number at epoch: | 60172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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