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 28415U 04035C 23156.71182368 .00003755 00000-0 22391-3 0 9995
2 28415 97.4689 194.0946 0045707 246.6920 112.9496 15.10891561 26883
Epoch (UTC): | 05 June 2023 17:05:01 |
Eccentricity: | 0.0045707 |
inclination: | 97.4689° |
perigee height: | 502 km |
apogee height: | 565 km |
right ascension of ascending node: | 194.0946° |
argument of perigee: | 246.6920° |
revolutions per day: | 15.10891561 |
mean anomaly at epoch: | 112.9496° |
orbit number at epoch: | 2688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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