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 28647U 05016B 25188.20020084 .00009457 00000-0 28127-3 0 9997
2 28647 56.9999 213.9841 0069063 271.9465 87.3676 15.33158297339299
| Epoch (UTC): | 07 July 2025 04:48:17 |
| Eccentricity: | 0.0069063 |
| inclination: | 56.9999° |
| perigee height: | 419 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 213.9841° |
| argument of perigee: | 271.9465° |
| revolutions per day: | 15.33158297 |
| mean anomaly at epoch: | 87.3676° |
| orbit number at epoch: | 33929 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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