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 25338U 98030A 23150.40892261 .00000220 00000-0 10970-3 0 9998
2 25338 98.6065 179.7690 0010460 12.8864 347.2581 14.26323197302728
Epoch (UTC): | 30 May 2023 09:48:50 |
Eccentricity: | 0.0010460 |
inclination: | 98.6065° |
perigee height: | 796 km |
apogee height: | 811 km |
right ascension of ascending node: | 179.7690° |
argument of perigee: | 12.8864° |
revolutions per day: | 14.26323197 |
mean anomaly at epoch: | 347.2581° |
orbit number at epoch: | 30272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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