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 37169U 10048B 23333.61332723 .00035594 00000-0 66225-3 0 9990
2 37169 97.9675 197.3279 0004635 123.2276 236.9418 15.48788182732940
| Epoch (UTC): | 29 November 2023 14:43:11 |
| Eccentricity: | 0.0004635 |
| inclination: | 97.9675° |
| perigee height: | 417 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 197.3279° |
| argument of perigee: | 123.2276° |
| revolutions per day: | 15.48788182 |
| mean anomaly at epoch: | 236.9418° |
| orbit number at epoch: | 73294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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