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 21799U 91076C 25197.78805056 .00003805 00000-0 32034-3 0 9995
2 21799 63.3007 323.3896 0891240 66.7981 302.4347 13.56728884 58013
| Epoch (UTC): | 16 July 2025 18:54:47 |
| Eccentricity: | 0.0891240 |
| inclination: | 63.3007° |
| perigee height: | 386 km |
| apogee height: | 1709 km |
| right ascension of ascending node: | 323.3896° |
| argument of perigee: | 66.7981° |
| revolutions per day: | 13.56728884 |
| mean anomaly at epoch: | 302.4347° |
| orbit number at epoch: | 5801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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