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 28654U 05018A 23343.18031425 .00000198 00000-0 12990-3 0 9990
2 28654 98.8953 56.5985 0013486 242.3906 117.5897 14.13074098956280
| Epoch (UTC): | 09 December 2023 04:19:39 |
| Eccentricity: | 0.0013486 |
| inclination: | 98.8953° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 56.5985° |
| argument of perigee: | 242.3906° |
| revolutions per day: | 14.13074098 |
| mean anomaly at epoch: | 117.5897° |
| orbit number at epoch: | 95628 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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