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 28375U 04025K 23088.39198985 .00000949 00000-0 28923-3 0 9998
2 28375 98.5166 27.5843 0083073 49.2894 311.5473 14.42332713986016
| Epoch (UTC): | 29 March 2023 09:24:27 |
| Eccentricity: | 0.0083073 |
| inclination: | 98.5166° |
| perigee height: | 691 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 27.5843° |
| argument of perigee: | 49.2894° |
| revolutions per day: | 14.42332713 |
| mean anomaly at epoch: | 311.5473° |
| orbit number at epoch: | 98601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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