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 30074U 99025QB 22181.03353886 .00000743 00000-0 47321-3 0 9993
2 30074 99.2224 210.8826 0109342 65.6655 295.5881 14.03987129789087
| Epoch (UTC): | 30 June 2022 00:48:17 |
| Eccentricity: | 0.0109342 |
| inclination: | 99.2224° |
| perigee height: | 800 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 210.8826° |
| argument of perigee: | 65.6655° |
| revolutions per day: | 14.03987129 |
| mean anomaly at epoch: | 295.5881° |
| orbit number at epoch: | 78908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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