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 26387U 00033D 23150.01775803 .00000749 00000-0 13294-3 0 9996
2 26387 97.7390 154.1587 0024600 237.9625 121.9192 14.69760527226798
| Epoch (UTC): | 30 May 2023 00:25:34 |
| Eccentricity: | 0.0024600 |
| inclination: | 97.7390° |
| perigee height: | 644 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 154.1587° |
| argument of perigee: | 237.9625° |
| revolutions per day: | 14.69760527 |
| mean anomaly at epoch: | 121.9192° |
| orbit number at epoch: | 22679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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