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 40930U 26150.60020661 +.00000000 +00000-0 +15532-3 0 00003
2 40930 5.9975 281.9566 0007619 146.6788 213.3820 14.82473346 04
| Epoch (UTC): | 30 May 2026 14:24:17 |
| Eccentricity: | 0.0007619 |
| inclination: | 5.9975° |
| perigee height: | 616 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 281.9566° |
| argument of perigee: | 146.6788° |
| revolutions per day: | 14.82473346 |
| mean anomaly at epoch: | 213.3820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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