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 00085U 61004C 21059.58993392 .00001637 00000-0 35600-3 0 9993
2 00085 38.7761 153.3555 0392438 47.2096 316.0965 14.21659482967544
Epoch (UTC): | 28 February 2021 14:09:30 |
Eccentricity: | 0.0392438 |
inclination: | 38.7761° |
perigee height: | 537 km |
apogee height: | 1102 km |
right ascension of ascending node: | 153.3555° |
argument of perigee: | 47.2096° |
revolutions per day: | 14.21659482 |
mean anomaly at epoch: | 316.0965° |
orbit number at epoch: | 96754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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