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 36605U 10030A 23160.50295451 .00001416 00000-0 70608-4 0 9994
2 36605 97.4460 167.9959 0001512 86.8080 273.3328 15.19155538719083
| Epoch (UTC): | 09 June 2023 12:04:15 |
| Eccentricity: | 0.0001512 |
| inclination: | 97.4460° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 167.9959° |
| argument of perigee: | 86.8080° |
| revolutions per day: | 15.19155538 |
| mean anomaly at epoch: | 273.3328° |
| orbit number at epoch: | 71908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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