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 02644U 66041D 23338.14374831 .00000550 00000-0 47224-3 0 9995
2 02644 90.1312 30.8546 0212481 290.9673 66.8874 13.76240128871272
| Epoch (UTC): | 04 December 2023 03:26:59 |
| Eccentricity: | 0.0212481 |
| inclination: | 90.1312° |
| perigee height: | 821 km |
| apogee height: | 1133 km |
| right ascension of ascending node: | 30.8546° |
| argument of perigee: | 290.9673° |
| revolutions per day: | 13.76240128 |
| mean anomaly at epoch: | 66.8874° |
| orbit number at epoch: | 87127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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