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 35868U 09049D 23082.91059731 .00000499 00000-0 23975-3 0 9993
2 35868 98.5527 50.5562 0005271 100.5574 259.6199 14.23159158701602
| Epoch (UTC): | 23 March 2023 21:51:15 |
| Eccentricity: | 0.0005271 |
| inclination: | 98.5527° |
| perigee height: | 811 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 50.5562° |
| argument of perigee: | 100.5574° |
| revolutions per day: | 14.23159158 |
| mean anomaly at epoch: | 259.6199° |
| orbit number at epoch: | 70160 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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