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 37398U 11018A 23271.91449066 .00000375 00000-0 00000-0 0 9990
2 37398 62.2200 220.6304 7180111 256.7690 20.8627 2.00716896 90851
| Epoch (UTC): | 28 September 2023 21:56:51 |
| Eccentricity: | 0.7180111 |
| inclination: | 62.2200° |
| perigee height: | 1108 km |
| apogee height: | 39229 km |
| right ascension of ascending node: | 220.6304° |
| argument of perigee: | 256.7690° |
| revolutions per day: | 2.00716896 |
| mean anomaly at epoch: | 20.8627° |
| orbit number at epoch: | 9085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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