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 26121.45245727 +.00000000 +00000-0 +00000-0 0 00007
2 24307 9.7537 54.4060 0006643 349.4044 173.2167 0.99996383 08
| Epoch (UTC): | 01 May 2026 10:51:32 |
| Eccentricity: | 0.0006643 |
| inclination: | 9.7537° |
| perigee height: | 35836 km |
| apogee height: | 35892 km |
| right ascension of ascending node: | 54.4060° |
| argument of perigee: | 349.4044° |
| revolutions per day: | 0.99996383 |
| mean anomaly at epoch: | 173.2167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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