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 24307U 26145.57614236 +.00000000 +00000-0 +00000-0 0 00001
2 24307 9.8074 54.1659 0006744 10.7842 196.8068 1.00003813 03
| Epoch (UTC): | 25 May 2026 13:49:38 |
| Eccentricity: | 0.0006744 |
| inclination: | 9.8074° |
| perigee height: | 35833 km |
| apogee height: | 35890 km |
| right ascension of ascending node: | 54.1659° |
| argument of perigee: | 10.7842° |
| revolutions per day: | 1.00003813 |
| mean anomaly at epoch: | 196.8068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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