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 28888U 05042A 24278.80549119 0.00032000 00000-0 41457-3 0 07
2 28888 97.0566 316.6704 0033770 164.2148 195.7851 15.58157707 04
| Epoch (UTC): | 04 October 2024 19:19:54 |
| Eccentricity: | 0.0033770 |
| inclination: | 97.0566° |
| perigee height: | 370 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 316.6704° |
| argument of perigee: | 164.2148° |
| revolutions per day: | 15.58157707 |
| mean anomaly at epoch: | 195.7851° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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