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 24665U 26150.02907394 +.00000000 +00000-0 +00000-0 0 00004
2 24665 11.9270 35.9106 0004180 125.1746 223.1753 0.98382167 05
| Epoch (UTC): | 30 May 2026 00:41:51 |
| Eccentricity: | 0.0004180 |
| inclination: | 11.9270° |
| perigee height: | 36307 km |
| apogee height: | 36343 km |
| right ascension of ascending node: | 35.9106° |
| argument of perigee: | 125.1746° |
| revolutions per day: | 0.98382167 |
| mean anomaly at epoch: | 223.1753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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