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 28075U 99057NF 23332.31724967 .00002152 00000-0 66012-3 0 9992
2 28075 98.7416 5.1267 0102459 92.8217 268.4702 14.39739403599915
| Epoch (UTC): | 28 November 2023 07:36:50 |
| Eccentricity: | 0.0102459 |
| inclination: | 98.7416° |
| perigee height: | 686 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 5.1267° |
| argument of perigee: | 92.8217° |
| revolutions per day: | 14.39739403 |
| mean anomaly at epoch: | 268.4702° |
| orbit number at epoch: | 59991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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