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 22176.53283776 .00011490 00000-0 31550-3 0 9993
2 39026 97.2672 167.1611 0032257 127.7977 232.6196 15.36860992530160
| Epoch (UTC): | 25 June 2022 12:47:17 |
| Eccentricity: | 0.0032257 |
| inclination: | 97.2672° |
| perigee height: | 433 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 167.1611° |
| argument of perigee: | 127.7977° |
| revolutions per day: | 15.36860992 |
| mean anomaly at epoch: | 232.6196° |
| orbit number at epoch: | 53016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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