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 15598U 85022B 23150.44813572 .00000026 00000-0 10581-4 0 9997
2 15598 82.9359 291.6562 0022935 148.2240 273.5464 13.76637546919221
| Epoch (UTC): | 30 May 2023 10:45:18 |
| Eccentricity: | 0.0022935 |
| inclination: | 82.9359° |
| perigee height: | 959 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 291.6562° |
| argument of perigee: | 148.2240° |
| revolutions per day: | 13.76637546 |
| mean anomaly at epoch: | 273.5464° |
| orbit number at epoch: | 91922 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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