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 35951U 09057A 23088.51229813 .00000632 00000-0 35702-3 0 9997
2 35951 98.7610 66.4231 0011218 1.7591 358.3619 14.13709323693404
| Epoch (UTC): | 29 March 2023 12:17:42 |
| Eccentricity: | 0.0011218 |
| inclination: | 98.7610° |
| perigee height: | 838 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 66.4231° |
| argument of perigee: | 1.7591° |
| revolutions per day: | 14.13709323 |
| mean anomaly at epoch: | 358.3619° |
| orbit number at epoch: | 69340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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