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 22627U 93024B 24279.11867601 .00001864 00000-0 24647-3 0 9996
2 22627 82.5214 142.5586 0021485 246.5919 113.3034 14.79356092696169
| Epoch (UTC): | 05 October 2024 02:50:53 |
| Eccentricity: | 0.0021485 |
| inclination: | 82.5214° |
| perigee height: | 616 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 142.5586° |
| argument of perigee: | 246.5919° |
| revolutions per day: | 14.79356092 |
| mean anomaly at epoch: | 113.3034° |
| orbit number at epoch: | 69616 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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