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 06787U 73054A 23160.85857404 .00000339 00000-0 14161-3 0 9991
2 06787 98.7107 15.3351 0027113 50.4580 309.8993 14.32376701593749
| Epoch (UTC): | 09 June 2023 20:36:20 |
| Eccentricity: | 0.0027113 |
| inclination: | 98.7107° |
| perigee height: | 764 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 15.3351° |
| argument of perigee: | 50.4580° |
| revolutions per day: | 14.32376701 |
| mean anomaly at epoch: | 309.8993° |
| orbit number at epoch: | 59374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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