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 23158.44821229 .00082656 00000-0 80364-3 0 9994
2 39026 97.2787 155.5538 0011205 307.2170 52.8067 15.65957587583779
| Epoch (UTC): | 07 June 2023 10:45:25 |
| Eccentricity: | 0.0011205 |
| inclination: | 97.2787° |
| perigee height: | 363 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 155.5538° |
| argument of perigee: | 307.2170° |
| revolutions per day: | 15.65957587 |
| mean anomaly at epoch: | 52.8067° |
| orbit number at epoch: | 58377 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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