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 26103.88348718 +.00000000 +00000-0 +12687-3 0 00004
2 42847 97.4022 268.5471 0010897 312.8756 47.1556 15.06069797 09
| Epoch (UTC): | 13 April 2026 21:12:13 |
| Eccentricity: | 0.0010897 |
| inclination: | 97.4022° |
| perigee height: | 541 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 268.5471° |
| argument of perigee: | 312.8756° |
| revolutions per day: | 15.06069797 |
| mean anomaly at epoch: | 47.1556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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