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 42946U 26145.47935824 +.00000000 +00000-0 +14095-3 0 00000
2 42946 34.9959 168.5643 0001606 131.0540 229.0307 15.02691596 03
| Epoch (UTC): | 25 May 2026 11:30:16 |
| Eccentricity: | 0.0001606 |
| inclination: | 34.9959° |
| perigee height: | 557 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 168.5643° |
| argument of perigee: | 131.0540° |
| revolutions per day: | 15.02691596 |
| mean anomaly at epoch: | 229.0307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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