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 24932U 26142.60497529 +.00000000 +00000-0 +00000-0 0 00000
2 24932 13.6837 15.1456 0008853 48.2660 289.1949 0.98308105 08
| Epoch (UTC): | 22 May 2026 14:31:09 |
| Eccentricity: | 0.0008853 |
| inclination: | 13.6837° |
| perigee height: | 36308 km |
| apogee height: | 36384 km |
| right ascension of ascending node: | 15.1456° |
| argument of perigee: | 48.2660° |
| revolutions per day: | 0.98308105 |
| mean anomaly at epoch: | 289.1949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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