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 60246U 24125J 24280.88102449 .00028722 00000-0 12255-2 0 9992
2 60246 97.2899 132.1210 0048997 243.8607 115.7584 15.21756753 12502
| Epoch (UTC): | 06 October 2024 21:08:40 |
| Eccentricity: | 0.0048997 |
| inclination: | 97.2899° |
| perigee height: | 467 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 132.1210° |
| argument of perigee: | 243.8607° |
| revolutions per day: | 15.21756753 |
| mean anomaly at epoch: | 115.7584° |
| orbit number at epoch: | 1250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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