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 10674U 78018A 25133.87089765 -.00000025 00000-0 40189-4 0 9990
2 10674 69.3636 336.4381 0164086 179.3419 278.4128 13.43696613316992
| Epoch (UTC): | 13 May 2025 20:54:05 |
| Eccentricity: | 0.0164086 |
| inclination: | 69.3636° |
| perigee height: | 973 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 336.4381° |
| argument of perigee: | 179.3419° |
| revolutions per day: | 13.43696613 |
| mean anomaly at epoch: | 278.4128° |
| orbit number at epoch: | 31699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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