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 24279.09716716 .00000112 00000-0 34809-3 0 9999
2 28096 63.6785 160.5816 0108844 162.5911 197.8894 13.40994116 19261
| Epoch (UTC): | 05 October 2024 02:19:55 |
| Eccentricity: | 0.0108844 |
| inclination: | 63.6785° |
| perigee height: | 1024 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 160.5816° |
| argument of perigee: | 162.5911° |
| revolutions per day: | 13.40994116 |
| mean anomaly at epoch: | 197.8894° |
| orbit number at epoch: | 1926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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