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 26150.45397072 +.00000000 +00000-0 +27628-3 0 00007
2 42847 97.4085 313.2996 0012893 143.3424 216.8688 15.06341815 00
| Epoch (UTC): | 30 May 2026 10:53:43 |
| Eccentricity: | 0.0012893 |
| inclination: | 97.4085° |
| perigee height: | 538 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 313.2996° |
| argument of perigee: | 143.3424° |
| revolutions per day: | 15.06341815 |
| mean anomaly at epoch: | 216.8688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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