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 36597U 10027B 23031.67700462 .00002869 00000-0 27646-3 0 9994
2 36597 97.9997 11.1010 0061074 60.9056 299.8259 14.92369835686420
| Epoch (UTC): | 31 January 2023 16:14:53 |
| Eccentricity: | 0.0061074 |
| inclination: | 97.9997° |
| perigee height: | 548 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 11.1010° |
| argument of perigee: | 60.9056° |
| revolutions per day: | 14.92369835 |
| mean anomaly at epoch: | 299.8259° |
| orbit number at epoch: | 68642 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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