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 24209U 26150.34100705 +.00000000 +00000-0 +00000-0 0 00004
2 24209 13.0436 24.6526 0017192 20.2752 211.6138 0.98446311 07
| Epoch (UTC): | 30 May 2026 08:11:03 |
| Eccentricity: | 0.0017192 |
| inclination: | 13.0436° |
| perigee height: | 36233 km |
| apogee height: | 36380 km |
| right ascension of ascending node: | 24.6526° |
| argument of perigee: | 20.2752° |
| revolutions per day: | 0.98446311 |
| mean anomaly at epoch: | 211.6138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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