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 6153U 72065A 23083.14937135 .00001753 00000-0 37738-3 0 9991
2 6153 35.0079 331.1518 0007333 319.1901 172.1766 14.58345637688405
| Epoch (UTC): | 24 March 2023 03:35:05 |
| Eccentricity: | 0.0007333 |
| inclination: | 35.0079° |
| perigee height: | 693 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 331.1518° |
| argument of perigee: | 319.1901° |
| revolutions per day: | 14.58345637 |
| mean anomaly at epoch: | 172.1766° |
| orbit number at epoch: | 68840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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