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 21797U 91081B 24284.53283007 .00000339 00000-0 32179-3 0 9993
2 21797 82.9528 237.1323 0038356 157.5550 254.2616 13.77749398652047
| Epoch (UTC): | 10 October 2024 12:47:16 |
| Eccentricity: | 0.0038356 |
| inclination: | 82.9528° |
| perigee height: | 943 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 237.1323° |
| argument of perigee: | 157.5550° |
| revolutions per day: | 13.77749398 |
| mean anomaly at epoch: | 254.2616° |
| orbit number at epoch: | 65204 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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