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 43678U 18084H 23086.17099261 .00002134 00000-0 21047-3 0 9990
2 43678 98.0081 228.5718 0010807 75.6326 284.6085 14.93081083240022
| Epoch (UTC): | 27 March 2023 04:06:13 |
| Eccentricity: | 0.0010807 |
| inclination: | 98.0081° |
| perigee height: | 581 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 228.5718° |
| argument of perigee: | 75.6326° |
| revolutions per day: | 14.93081083 |
| mean anomaly at epoch: | 284.6085° |
| orbit number at epoch: | 24002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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