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 21397U 91039A 24256.16432373 .00008359 00000-0 67991-3 0 9992
2 21397 82.5199 141.5246 0016715 22.4773 337.7179 14.99332310804505
| Epoch (UTC): | 12 September 2024 03:56:37 |
| Eccentricity: | 0.0016715 |
| inclination: | 82.5199° |
| perigee height: | 557 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 141.5246° |
| argument of perigee: | 22.4773° |
| revolutions per day: | 14.99332310 |
| mean anomaly at epoch: | 337.7179° |
| orbit number at epoch: | 80450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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