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 39026U 12072A 23159.53446751 .00088572 00000-0 85393-3 0 9998
2 39026 97.2791 156.6773 0011182 301.2994 58.7170 15.66149161583940
| Epoch (UTC): | 08 June 2023 12:49:37 |
| Eccentricity: | 0.0011182 |
| inclination: | 97.2791° |
| perigee height: | 362 km |
| apogee height: | 377 km |
| right ascension of ascending node: | 156.6773° |
| argument of perigee: | 301.2994° |
| revolutions per day: | 15.66149161 |
| mean anomaly at epoch: | 58.7170° |
| orbit number at epoch: | 58394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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