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 46U 60007B 22175.54780527 .00000274 00000-0 75709-4 0 9993
2 46 66.6887 214.4524 0215878 300.5445 57.4513 14.49709308245929
| Epoch (UTC): | 24 June 2022 13:08:50 |
| Eccentricity: | 0.0215878 |
| inclination: | 66.6887° |
| perigee height: | 573 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 214.4524° |
| argument of perigee: | 300.5445° |
| revolutions per day: | 14.49709308 |
| mean anomaly at epoch: | 57.4513° |
| orbit number at epoch: | 24592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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