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 40021U 14033M 23091.83981142 .00012901 00000-0 11346-2 0 9999
2 40021 98.0503 53.4527 0012080 155.7177 204.4615 14.96612506477767
| Epoch (UTC): | 01 April 2023 20:09:19 |
| Eccentricity: | 0.0012080 |
| inclination: | 98.0503° |
| perigee height: | 569 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 53.4527° |
| argument of perigee: | 155.7177° |
| revolutions per day: | 14.96612506 |
| mean anomaly at epoch: | 204.4615° |
| orbit number at epoch: | 47776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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