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 41246U 00055EW 23027.45301821 .00009125 00000-0 30016-2 0 9994
2 41246 98.9854 208.8805 0060299 39.2369 321.3164 14.37407630368542
| Epoch (UTC): | 27 January 2023 10:52:20 |
| Eccentricity: | 0.0060299 |
| inclination: | 98.9854° |
| perigee height: | 724 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 208.8805° |
| argument of perigee: | 39.2369° |
| revolutions per day: | 14.37407630 |
| mean anomaly at epoch: | 321.3164° |
| orbit number at epoch: | 36854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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