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 48274U 21035A 23266.58410175 .00023510 00000-0 25648-3 0 9995
2 48274 41.4733 277.2231 0007978 91.5733 268.6020 15.62779368137214
Epoch (UTC): | 23 September 2023 14:01:06 |
Eccentricity: | 0.0007978 |
inclination: | 41.4733° |
perigee height: | 374 km |
apogee height: | 385 km |
right ascension of ascending node: | 277.2231° |
argument of perigee: | 91.5733° |
revolutions per day: | 15.62779368 |
mean anomaly at epoch: | 268.6020° |
orbit number at epoch: | 13721 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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