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 23080.96002059 .00000197 00000-0 00000+0 0 9991
2 37398 62.2724 246.8704 7207328 255.6449 352.2347 2.00514835 87032
| Epoch (UTC): | 21 March 2023 23:02:25 |
| Eccentricity: | 0.7207328 |
| inclination: | 62.2724° |
| perigee height: | 1040 km |
| apogee height: | 39332 km |
| right ascension of ascending node: | 246.8704° |
| argument of perigee: | 255.6449° |
| revolutions per day: | 2.00514835 |
| mean anomaly at epoch: | 352.2347° |
| orbit number at epoch: | 8703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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