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 37841U 11058D 25131.88861492 .00000453 00000-0 10222-3 0 9998
2 37841 19.9734 328.1721 0011793 109.3219 286.7837 14.11426795701276
Epoch (UTC): | 11 May 2025 21:19:36 |
Eccentricity: | 0.0011793 |
inclination: | 19.9734° |
perigee height: | 846 km |
apogee height: | 863 km |
right ascension of ascending node: | 328.1721° |
argument of perigee: | 109.3219° |
revolutions per day: | 14.11426795 |
mean anomaly at epoch: | 286.7837° |
orbit number at epoch: | 70127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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