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 28096U 03054B 25163.20835989 -.00000033 00000-0 96559-4 0 9993
2 28096 63.6797 249.1544 0089046 144.2495 216.4538 13.41035979 52806
| Epoch (UTC): | 12 June 2025 05:00:02 |
| Eccentricity: | 0.0089046 |
| inclination: | 63.6797° |
| perigee height: | 1039 km |
| apogee height: | 1172 km |
| right ascension of ascending node: | 249.1544° |
| argument of perigee: | 144.2495° |
| revolutions per day: | 13.41035979 |
| mean anomaly at epoch: | 216.4538° |
| orbit number at epoch: | 5280 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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