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 31129U 07012N 25107.88824413 .00004218 00000-0 77357-3 0 9996
2 31129 98.4038 72.1489 0083327 309.9132 49.4766 14.64087308956468
Epoch (UTC): | 17 April 2025 21:19:04 |
Eccentricity: | 0.0083327 |
inclination: | 98.4038° |
perigee height: | 621 km |
apogee height: | 739 km |
right ascension of ascending node: | 72.1489° |
argument of perigee: | 309.9132° |
revolutions per day: | 14.64087308 |
mean anomaly at epoch: | 49.4766° |
orbit number at epoch: | 95646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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