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 18421U 87088A 23160.72877134 .00009148 00000-0 36809-3 0 9999
2 18421 82.4968 274.2788 0011962 233.8569 126.1562 15.24687284949606
Epoch (UTC): | 09 June 2023 17:29:25 |
Eccentricity: | 0.0011962 |
inclination: | 82.4968° |
perigee height: | 483 km |
apogee height: | 500 km |
right ascension of ascending node: | 274.2788° |
argument of perigee: | 233.8569° |
revolutions per day: | 15.24687284 |
mean anomaly at epoch: | 126.1562° |
orbit number at epoch: | 94960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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