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 30336U 99025AAX 22181.62689198 .00000200 00000-0 12099-3 0 9999
2 30336 98.7293 217.5000 0045804 33.6294 90.0900 14.16594340797321
Epoch (UTC): | 30 June 2022 15:02:43 |
Eccentricity: | 0.0045804 |
inclination: | 98.7293° |
perigee height: | 804 km |
apogee height: | 870 km |
right ascension of ascending node: | 217.5000° |
argument of perigee: | 33.6294° |
revolutions per day: | 14.16594340 |
mean anomaly at epoch: | 90.0900° |
orbit number at epoch: | 79732 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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