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 27518U 02042D 22144.88470792 .00000273 00000-0 11526-2 0 9998
2 27518 28.8382 33.7643 7132270 127.3548 320.8676 2.36569961170146
Epoch (UTC): | 24 May 2022 21:13:58 |
Eccentricity: | 0.7132270 |
inclination: | 28.8382° |
perigee height: | 445 km |
apogee height: | 34382 km |
right ascension of ascending node: | 33.7643° |
argument of perigee: | 127.3548° |
revolutions per day: | 2.36569961 |
mean anomaly at epoch: | 320.8676° |
orbit number at epoch: | 17014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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