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 37380U 10062M 25143.51889576 .00001000 00000-0 12793-3 0 9990
2 37380 71.9717 294.8866 0014116 131.7549 228.4826 14.83650179307962
Epoch (UTC): | 23 May 2025 12:27:12 |
Eccentricity: | 0.0014116 |
inclination: | 71.9717° |
perigee height: | 608 km |
apogee height: | 628 km |
right ascension of ascending node: | 294.8866° |
argument of perigee: | 131.7549° |
revolutions per day: | 14.83650179 |
mean anomaly at epoch: | 228.4826° |
orbit number at epoch: | 30796 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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