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 56372U 26142.74951110 +.00000000 +00000-0 +00000-0 0 00009
2 56372 2.6612 80.1187 0004085 279.8154 239.0757 1.00281652 08
| Epoch (UTC): | 22 May 2026 17:59:17 |
| Eccentricity: | 0.0004085 |
| inclination: | 2.6612° |
| perigee height: | 35767 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 80.1187° |
| argument of perigee: | 279.8154° |
| revolutions per day: | 1.00281652 |
| mean anomaly at epoch: | 239.0757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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