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 25139.63172710 .00043872 00000-0 49835-3 0 9990
2 18421 82.4817 269.0705 0006401 217.0566 143.0250 15.62118773 58655
Epoch (UTC): | 19 May 2025 15:09:41 |
Eccentricity: | 0.0006401 |
inclination: | 82.4817° |
perigee height: | 377 km |
apogee height: | 386 km |
right ascension of ascending node: | 269.0705° |
argument of perigee: | 217.0566° |
revolutions per day: | 15.62118773 |
mean anomaly at epoch: | 143.0250° |
orbit number at epoch: | 5865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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