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 25544U 98067A 23339.01611087 .00032187 00000-0 56578-3 0 9999
2 25544 51.6402 202.4175 0001285 358.1544 143.2048 15.50194500428283
| Epoch (UTC): | 05 December 2023 00:23:11 |
| Eccentricity: | 0.0001285 |
| inclination: | 51.6402° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 202.4175° |
| argument of perigee: | 358.1544° |
| revolutions per day: | 15.50194500 |
| mean anomaly at epoch: | 143.2048° |
| orbit number at epoch: | 42828 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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