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 23092.15327164 .00000381 00000-0 22855-3 0 9991
2 28654 98.9137 166.9023 0013563 231.9838 128.0110 14.12902674920834
| Epoch (UTC): | 02 April 2023 03:40:42 |
| Eccentricity: | 0.0013563 |
| inclination: | 98.9137° |
| perigee height: | 839 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 166.9023° |
| argument of perigee: | 231.9838° |
| revolutions per day: | 14.12902674 |
| mean anomaly at epoch: | 128.0110° |
| orbit number at epoch: | 92083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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