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 28538U 05004B 21057.16990874 0.00000000 00000-0 00000-0 0 07
2 28538 63.8280 133.9218 0122816 21.5609 338.4391 13.43141061 00
Epoch (UTC): | 26 February 2021 04:04:40 |
Eccentricity: | 0.0122816 |
inclination: | 63.8280° |
perigee height: | 1006 km |
apogee height: | 1189 km |
right ascension of ascending node: | 133.9218° |
argument of perigee: | 21.5609° |
revolutions per day: | 13.43141061 |
mean anomaly at epoch: | 338.4391° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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