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 23028.25681773 .00000661 00000-0 15311-3 0 9994
2 46 66.6916 345.6412 0203274 140.7278 220.8779 14.50066291277485
| Epoch (UTC): | 28 January 2023 06:09:49 |
| Eccentricity: | 0.0203274 |
| inclination: | 66.6916° |
| perigee height: | 581 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 345.6412° |
| argument of perigee: | 140.7278° |
| revolutions per day: | 14.50066291 |
| mean anomaly at epoch: | 220.8779° |
| orbit number at epoch: | 27748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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