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 37794U 11044G 23081.85226488 .00001083 00000-0 22186-3 0 9991
2 37794 97.8118 108.0577 0011755 325.8672 207.1242 14.62542672618604
| Epoch (UTC): | 22 March 2023 20:27:15 |
| Eccentricity: | 0.0011755 |
| inclination: | 97.8118° |
| perigee height: | 676 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 108.0577° |
| argument of perigee: | 325.8672° |
| revolutions per day: | 14.62542672 |
| mean anomaly at epoch: | 207.1242° |
| orbit number at epoch: | 61860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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