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 21949U 92023A 21056.89303536 0.00000020 00000-0 75427-5 0 07
2 21949 85.0126 110.9726 0005695 116.8310 243.1688 14.31470291 04
| Epoch (UTC): | 25 February 2021 21:25:58 |
| Eccentricity: | 0.0005695 |
| inclination: | 85.0126° |
| perigee height: | 783 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 110.9726° |
| argument of perigee: | 116.8310° |
| revolutions per day: | 14.31470291 |
| mean anomaly at epoch: | 243.1688° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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