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 28373U 04025H 25131.83045595 .00000595 00000-0 16688-3 0 9996
2 28373 98.6833 124.8673 0066834 124.1227 236.6329 14.48495974100938
| Epoch (UTC): | 11 May 2025 19:55:51 |
| Eccentricity: | 0.0066834 |
| inclination: | 98.6833° |
| perigee height: | 683 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 124.8673° |
| argument of perigee: | 124.1227° |
| revolutions per day: | 14.48495974 |
| mean anomaly at epoch: | 236.6329° |
| orbit number at epoch: | 10093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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