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 00085U 61004C 22219.41282336 .00002792 00000-0 54644-3 0 9995
2 00085 38.7701 343.7445 0373353 322.0284 35.4676 14.27630193 42368
| Epoch (UTC): | 07 August 2022 09:54:27 |
| Eccentricity: | 0.0373353 |
| inclination: | 38.7701° |
| perigee height: | 531 km |
| apogee height: | 1067 km |
| right ascension of ascending node: | 343.7445° |
| argument of perigee: | 322.0284° |
| revolutions per day: | 14.27630193 |
| mean anomaly at epoch: | 35.4676° |
| orbit number at epoch: | 4236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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