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 26932U 01043D 23334.45990667 .00000414 00000-0 18968-3 0 9995
2 26932 67.0544 133.6268 0007455 250.0844 109.9454 14.30665352157496
| Epoch (UTC): | 30 November 2023 11:02:15 |
| Eccentricity: | 0.0007455 |
| inclination: | 67.0544° |
| perigee height: | 784 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 133.6268° |
| argument of perigee: | 250.0844° |
| revolutions per day: | 14.30665352 |
| mean anomaly at epoch: | 109.9454° |
| orbit number at epoch: | 15749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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