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 37813U 11050A 22246.99566080 0.00001250 00000-0 11441-3 0 03
2 37813 97.8793 13.8280 0001856 37.9612 322.0387 14.95031690 00
| Epoch (UTC): | 03 September 2022 23:53:45 |
| Eccentricity: | 0.0001856 |
| inclination: | 97.8793° |
| perigee height: | 581 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 13.8280° |
| argument of perigee: | 37.9612° |
| revolutions per day: | 14.95031690 |
| mean anomaly at epoch: | 322.0387° |
| 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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