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 37253U 10066K 22227.75451636 .00003484 00000-0 36648-3 0 9994
2 37253 34.5126 21.1553 4198325 21.1610 352.0646 7.03200162291709
| Epoch (UTC): | 15 August 2022 18:06:30 |
| Eccentricity: | 0.4198325 |
| inclination: | 34.5126° |
| perigee height: | 298 km |
| apogee height: | 9962 km |
| right ascension of ascending node: | 21.1553° |
| argument of perigee: | 21.1610° |
| revolutions per day: | 7.03200162 |
| mean anomaly at epoch: | 352.0646° |
| orbit number at epoch: | 29170 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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