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 26052U 00001A 23080.65078345 .00000027 00000-0 00000+0 0 9995
2 26052 9.9794 40.7071 0001484 283.8392 268.7969 1.00273465 19753
| Epoch (UTC): | 21 March 2023 15:37:07 |
| Eccentricity: | 0.0001484 |
| inclination: | 9.9794° |
| perigee height: | 35779 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 40.7071° |
| argument of perigee: | 283.8392° |
| revolutions per day: | 1.00273465 |
| mean anomaly at epoch: | 268.7969° |
| orbit number at epoch: | 1975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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