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 07003U 73107A 22228.83632698 .00005537 00000-0 20030-3 0 9997
2 07003 73.9213 242.2753 0354446 156.5779 205.2010 14.85524715492230
Epoch (UTC): | 16 August 2022 20:04:18 |
Eccentricity: | 0.0354446 |
inclination: | 73.9213° |
perigee height: | 364 km |
apogee height: | 860 km |
right ascension of ascending node: | 242.2753° |
argument of perigee: | 156.5779° |
revolutions per day: | 14.85524715 |
mean anomaly at epoch: | 205.2010° |
orbit number at epoch: | 49223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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