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 42846U 26103.88157132 +.00000000 +00000-0 +14686-3 0 00002
2 42846 97.3989 267.7739 0012504 337.4994 22.5684 15.05891383 03
| Epoch (UTC): | 13 April 2026 21:09:27 |
| Eccentricity: | 0.0012504 |
| inclination: | 97.3989° |
| perigee height: | 540 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 267.7739° |
| argument of perigee: | 337.4994° |
| revolutions per day: | 15.05891383 |
| mean anomaly at epoch: | 22.5684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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