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 37855U 11061F 24182.03846730 .16796037 55665-5 20608-3 0 9995
2 37855 101.6644 19.4898 0012765 270.0453 89.9372 16.49099678695123
| Epoch (UTC): | 30 June 2024 00:55:23 |
| Eccentricity: | 0.0012765 |
| inclination: | 101.6644° |
| perigee height: | 133 km |
| apogee height: | 150 km |
| right ascension of ascending node: | 19.4898° |
| argument of perigee: | 270.0453° |
| revolutions per day: | 16.49099678 |
| mean anomaly at epoch: | 89.9372° |
| orbit number at epoch: | 69512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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