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 40057U 14034E 25013.10175562 .00006429 00000-0 66294-3 0 9997
2 40057 98.3139 244.7570 0008131 172.1723 187.9622 14.90569158568929
Epoch (UTC): | 13 January 2025 02:26:31 |
Eccentricity: | 0.0008131 |
inclination: | 98.3139° |
perigee height: | 590 km |
apogee height: | 602 km |
right ascension of ascending node: | 244.7570° |
argument of perigee: | 172.1723° |
revolutions per day: | 14.90569158 |
mean anomaly at epoch: | 187.9622° |
orbit number at epoch: | 56892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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