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 37089U 93036BFK 24355.55281554 .00013363 00000-0 33874-2 0 9995
2 37089 74.0407 95.0022 0159192 285.2435 73.1169 14.43502540609386
Epoch (UTC): | 20 December 2024 13:16:03 |
Eccentricity: | 0.0159192 |
inclination: | 74.0407° |
perigee height: | 633 km |
apogee height: | 860 km |
right ascension of ascending node: | 95.0022° |
argument of perigee: | 285.2435° |
revolutions per day: | 14.43502540 |
mean anomaly at epoch: | 73.1169° |
orbit number at epoch: | 60938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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