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 25682U 99020A 24306.62765522 .00002113 00000-0 43870-3 0 9995
2 25682 97.8783 326.9023 0001129 87.9612 23.4678 14.61097491359209
Epoch (UTC): | 01 November 2024 15:03:49 |
Eccentricity: | 0.0001129 |
inclination: | 97.8783° |
perigee height: | 689 km |
apogee height: | 690 km |
right ascension of ascending node: | 326.9023° |
argument of perigee: | 87.9612° |
revolutions per day: | 14.61097491 |
mean anomaly at epoch: | 23.4678° |
orbit number at epoch: | 35920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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