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 20491U 90013D 25193.89046751 .00000374 00000-0 76892-3 0 9998
2 20491 99.0138 183.2663 0466943 233.7815 121.9272 13.03717735684816
| Epoch (UTC): | 12 July 2025 21:22:16 |
| Eccentricity: | 0.0466943 |
| inclination: | 99.0138° |
| perigee height: | 891 km |
| apogee height: | 1603 km |
| right ascension of ascending node: | 183.2663° |
| argument of perigee: | 233.7815° |
| revolutions per day: | 13.03717735 |
| mean anomaly at epoch: | 121.9272° |
| orbit number at epoch: | 68481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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