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 32953U 08025A 23332.54755172 .00000055 00000-0 32650-3 0 9995
2 32953 82.5048 214.8665 0018874 183.8216 176.2722 12.43132543703937
Epoch (UTC): | 28 November 2023 13:08:28 |
Eccentricity: | 0.0018874 |
inclination: | 82.5048° |
perigee height: | 1478 km |
apogee height: | 1508 km |
right ascension of ascending node: | 214.8665° |
argument of perigee: | 183.8216° |
revolutions per day: | 12.43132543 |
mean anomaly at epoch: | 176.2722° |
orbit number at epoch: | 70393 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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