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 40024U 26145.33101216 +.00000000 +00000-0 +55288-3 0 00009
2 40024 98.0745 175.7068 0001994 243.3155 116.7880 15.30617735 04
| Epoch (UTC): | 25 May 2026 07:56:39 |
| Eccentricity: | 0.0001994 |
| inclination: | 98.0745° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 175.7068° |
| argument of perigee: | 243.3155° |
| revolutions per day: | 15.30617735 |
| mean anomaly at epoch: | 116.7880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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