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 48726U 02032BK 24226.35335040 .00083648 00000-0 92425-2 0 9996
2 48726 98.9425 274.6563 0034584 198.5717 161.4236 14.86550014176686
| Epoch (UTC): | 13 August 2024 08:28:49 |
| Eccentricity: | 0.0034584 |
| inclination: | 98.9425° |
| perigee height: | 584 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 274.6563° |
| argument of perigee: | 198.5717° |
| revolutions per day: | 14.86550014 |
| mean anomaly at epoch: | 161.4236° |
| orbit number at epoch: | 17668 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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