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 28895U 05043F 23334.06159019 .00003793 00000-0 69252-3 0 9999
2 28895 98.1760 105.1652 0014991 269.2140 90.7346 14.66479971965343
| Epoch (UTC): | 30 November 2023 01:28:41 |
| Eccentricity: | 0.0014991 |
| inclination: | 98.1760° |
| perigee height: | 662 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 105.1652° |
| argument of perigee: | 269.2140° |
| revolutions per day: | 14.66479971 |
| mean anomaly at epoch: | 90.7346° |
| orbit number at epoch: | 96534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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