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 26065U 00004E 23081.16564602 .00000323 00000-0 12753-3 0 9996
2 26065 100.1975 146.2330 0037160 134.4233 225.9999 14.37155052213576
| Epoch (UTC): | 22 March 2023 03:58:31 |
| Eccentricity: | 0.0037160 |
| inclination: | 100.1975° |
| perigee height: | 741 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 146.2330° |
| argument of perigee: | 134.4233° |
| revolutions per day: | 14.37155052 |
| mean anomaly at epoch: | 225.9999° |
| orbit number at epoch: | 21357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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