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 28355U 04021D 24280.46890885 .00000386 00000-0 42036-3 0 9999
2 28355 70.9660 299.1837 0225448 115.5146 354.2966 13.68054470 14031
| Epoch (UTC): | 06 October 2024 11:15:13 |
| Eccentricity: | 0.0225448 |
| inclination: | 70.9660° |
| perigee height: | 840 km |
| apogee height: | 1173 km |
| right ascension of ascending node: | 299.1837° |
| argument of perigee: | 115.5146° |
| revolutions per day: | 13.68054470 |
| mean anomaly at epoch: | 354.2966° |
| orbit number at epoch: | 1403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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