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 23435U 94084A 23081.48035625 -.00000291 00000-0 00000+0 0 9991
2 23435 14.5720 3.5639 0001358 283.2175 225.1171 0.99084328 19832
| Epoch (UTC): | 22 March 2023 11:31:42 |
| Eccentricity: | 0.0001358 |
| inclination: | 14.5720° |
| perigee height: | 36116 km |
| apogee height: | 36128 km |
| right ascension of ascending node: | 3.5639° |
| argument of perigee: | 283.2175° |
| revolutions per day: | 0.99084328 |
| mean anomaly at epoch: | 225.1171° |
| orbit number at epoch: | 1983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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