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 26474U 00047B 23032.24441455 .00002123 00000-0 18480-3 0 9995
2 26474 67.9956 314.4592 0057620 226.4917 133.1431 14.97791984222692
| Epoch (UTC): | 01 February 2023 05:51:57 |
| Eccentricity: | 0.0057620 |
| inclination: | 67.9956° |
| perigee height: | 533 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 314.4592° |
| argument of perigee: | 226.4917° |
| revolutions per day: | 14.97791984 |
| mean anomaly at epoch: | 133.1431° |
| orbit number at epoch: | 22269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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