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 42847U 26145.40535904 +.00000000 +00000-0 +26086-3 0 00001
2 42847 97.4075 308.4460 0012369 160.7800 199.3897 15.06293122 04
| Epoch (UTC): | 25 May 2026 09:43:43 |
| Eccentricity: | 0.0012369 |
| inclination: | 97.4075° |
| perigee height: | 539 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 308.4460° |
| argument of perigee: | 160.7800° |
| revolutions per day: | 15.06293122 |
| mean anomaly at epoch: | 199.3897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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