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 25682U 99020A 21135.89471375 -.00000131 00000-0 -19389-4 0 9990
2 25682 98.0318 193.9112 0001168 100.1936 259.9368 14.57200637174656
| Epoch (UTC): | 15 May 2021 21:28:23 |
| Eccentricity: | 0.0001168 |
| inclination: | 98.0318° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 193.9112° |
| argument of perigee: | 100.1936° |
| revolutions per day: | 14.57200637 |
| mean anomaly at epoch: | 259.9368° |
| orbit number at epoch: | 17465 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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