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 00059U 60013B 23150.92185702 .00000113 00000-0 34539-4 0 9992
2 00059 28.2490 83.3329 0189002 329.9179 29.0627 13.53029912 92270
| Epoch (UTC): | 30 May 2023 22:07:28 |
| Eccentricity: | 0.0189002 |
| inclination: | 28.2490° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 83.3329° |
| argument of perigee: | 329.9179° |
| revolutions per day: | 13.53029912 |
| mean anomaly at epoch: | 29.0627° |
| orbit number at epoch: | 9227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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