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 28541U 05004C 23151.19127270 0.00000000 00000-0 00000-0 0 03
2 28541 63.4091 38.0191 0457687 0.0773 359.9378 13.40874094 05
| Epoch (UTC): | 31 May 2023 04:35:25 |
| Eccentricity: | 0.0457687 |
| inclination: | 63.4091° |
| perigee height: | 763 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 38.0191° |
| argument of perigee: | 0.0773° |
| revolutions per day: | 13.40874094 |
| mean anomaly at epoch: | 359.9378° |
| 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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