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 07665U 75012B 22176.89825807 .00000011 00000-0 26562-3 0 9990
2 07665 69.2303 25.6076 0023400 331.4940 122.0180 12.70416162196547
| Epoch (UTC): | 25 June 2022 21:33:29 |
| Eccentricity: | 0.0023400 |
| inclination: | 69.2303° |
| perigee height: | 1362 km |
| apogee height: | 1398 km |
| right ascension of ascending node: | 25.6076° |
| argument of perigee: | 331.4940° |
| revolutions per day: | 12.70416162 |
| mean anomaly at epoch: | 122.0180° |
| orbit number at epoch: | 19654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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