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 38528U 12034A 23310.90411248 0.00000000 00000-0 00000-0 0 07
2 38528 5.0574 66.9107 0012697 6.0358 354.0056 1.00270000 08
| Epoch (UTC): | 06 November 2023 21:41:55 |
| Eccentricity: | 0.0012697 |
| inclination: | 5.0574° |
| perigee height: | 35733 km |
| apogee height: | 35840 km |
| right ascension of ascending node: | 66.9107° |
| argument of perigee: | 6.0358° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 354.0056° |
| 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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