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 21263U 91032A 23151.92692324 .00000100 00000-0 59763-4 0 9993
2 21263 98.5315 147.3264 0014494 43.6483 316.5841 14.26120767666398
| Epoch (UTC): | 31 May 2023 22:14:46 |
| Eccentricity: | 0.0014494 |
| inclination: | 98.5315° |
| perigee height: | 794 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 147.3264° |
| argument of perigee: | 43.6483° |
| revolutions per day: | 14.26120767 |
| mean anomaly at epoch: | 316.5841° |
| orbit number at epoch: | 66639 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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