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 42947U 26145.50558838 +.00000000 +00000-0 +15319-3 0 00001
2 42947 34.9960 159.3072 0004646 358.3874 1.6819 15.04368091 06
| Epoch (UTC): | 25 May 2026 12:08:02 |
| Eccentricity: | 0.0004646 |
| inclination: | 34.9960° |
| perigee height: | 550 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 159.3072° |
| argument of perigee: | 358.3874° |
| revolutions per day: | 15.04368091 |
| mean anomaly at epoch: | 1.6819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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