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 24297U 26101.43788235 +.00000000 +00000-0 +17416-3 0 00009
2 24297 70.9009 115.4304 0022074 51.6683 308.6418 14.13823787 07
| Epoch (UTC): | 11 April 2026 10:30:33 |
| Eccentricity: | 0.0022074 |
| inclination: | 70.9009° |
| perigee height: | 830 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 115.4304° |
| argument of perigee: | 51.6683° |
| revolutions per day: | 14.13823787 |
| mean anomaly at epoch: | 308.6418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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