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 23032.91866898 .00012442 00000-0 14765-3 0 9990
2 48274 41.4750 260.6450 0002270 112.6872 75.5247 15.61002378100676
Epoch (UTC): | 01 February 2023 22:02:53 |
Eccentricity: | 0.0002270 |
inclination: | 41.4750° |
perigee height: | 383 km |
apogee height: | 386 km |
right ascension of ascending node: | 260.6450° |
argument of perigee: | 112.6872° |
revolutions per day: | 15.61002378 |
mean anomaly at epoch: | 75.5247° |
orbit number at epoch: | 10067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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