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 25261U 98017B 24278.04485601 .00002788 00000-0 98673-3 0 9993
2 25261 98.8524 282.3030 0004104 140.6475 219.5008 14.35413146387092
| Epoch (UTC): | 04 October 2024 01:04:35 |
| Eccentricity: | 0.0004104 |
| inclination: | 98.8524° |
| perigee height: | 771 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 282.3030° |
| argument of perigee: | 140.6475° |
| revolutions per day: | 14.35413146 |
| mean anomaly at epoch: | 219.5008° |
| orbit number at epoch: | 38709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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