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 42400U 00055SU 23150.93271247 .00002540 00000-0 13375-2 0 9998
2 42400 98.7049 203.7077 0023363 17.7788 342.4198 14.14720591368608
| Epoch (UTC): | 30 May 2023 22:23:06 |
| Eccentricity: | 0.0023363 |
| inclination: | 98.7049° |
| perigee height: | 826 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 203.7077° |
| argument of perigee: | 17.7788° |
| revolutions per day: | 14.14720591 |
| mean anomaly at epoch: | 342.4198° |
| orbit number at epoch: | 36860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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