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 27421U 02021A 24282.57901924 .00003867 00000-0 83258-3 0 9999
2 27421 98.0747 335.0316 0132387 31.8188 329.0921 14.53668124173228
| Epoch (UTC): | 08 October 2024 13:53:47 |
| Eccentricity: | 0.0132387 |
| inclination: | 98.0747° |
| perigee height: | 620 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 335.0316° |
| argument of perigee: | 31.8188° |
| revolutions per day: | 14.53668124 |
| mean anomaly at epoch: | 329.0921° |
| orbit number at epoch: | 17322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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