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 28537U 05004A 22113.83463640 0.00000000 00000-0 00000-0 0 00
2 28537 63.4140 346.7364 0423104 359.2122 0.7878 13.40829774 01
| Epoch (UTC): | 23 April 2022 20:01:52 |
| Eccentricity: | 0.0423104 |
| inclination: | 63.4140° |
| perigee height: | 789 km |
| apogee height: | 1423 km |
| right ascension of ascending node: | 346.7364° |
| argument of perigee: | 359.2122° |
| revolutions per day: | 13.40829774 |
| mean anomaly at epoch: | 0.7878° |
| 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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