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 is defined by the following mean orbital elements,
1 24674U 26144.81277756 +.00000000 +00000-0 +00000-0 0 00006
2 24674 10.2689 49.8752 0003825 357.7220 194.6919 0.99974458 04
| Epoch (UTC): | 24 May 2026 19:30:23 |
| Eccentricity: | 0.0003825 |
| inclination: | 10.2689° |
| perigee height: | 35854 km |
| apogee height: | 35886 km |
| right ascension of ascending node: | 49.8752° |
| argument of perigee: | 357.7220° |
| revolutions per day: | 0.99974458 |
| mean anomaly at epoch: | 194.6919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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