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 27652U 03004B 24358.12779056 .00004184 00000-0 42265-3 0 9997
2 27652 40.0027 280.9766 0022194 250.8348 109.0040 14.91492834188537
| Epoch (UTC): | 23 December 2024 03:04:01 |
| Eccentricity: | 0.0022194 |
| inclination: | 40.0027° |
| perigee height: | 578 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 280.9766° |
| argument of perigee: | 250.8348° |
| revolutions per day: | 14.91492834 |
| mean anomaly at epoch: | 109.0040° |
| orbit number at epoch: | 18853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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