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 22077U 92052B 23080.83765726 -.00000053 00000-0 34744-4 0 9998
2 22077 66.0832 240.0938 0004444 194.6125 271.7740 12.86556492437454
| Epoch (UTC): | 21 March 2023 20:06:13 |
| Eccentricity: | 0.0004444 |
| inclination: | 66.0832° |
| perigee height: | 1312 km |
| apogee height: | 1318 km |
| right ascension of ascending node: | 240.0938° |
| argument of perigee: | 194.6125° |
| revolutions per day: | 12.86556492 |
| mean anomaly at epoch: | 271.7740° |
| orbit number at epoch: | 43745 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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