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 01778U 65096A 23148.24656996 .00000836 00000-0 21984-3 0 9998
2 01778 34.2592 226.4227 0749067 245.5978 106.4747 13.47619508814059
| Epoch (UTC): | 28 May 2023 05:55:03 |
| Eccentricity: | 0.0749067 |
| inclination: | 34.2592° |
| perigee height: | 522 km |
| apogee height: | 1640 km |
| right ascension of ascending node: | 226.4227° |
| argument of perigee: | 245.5978° |
| revolutions per day: | 13.47619508 |
| mean anomaly at epoch: | 106.4747° |
| orbit number at epoch: | 81405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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