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 56479U 26144.86632204 +.00000000 +00000-0 +70542-4 0 00004
2 56479 69.9990 292.2278 0002808 277.4765 82.6075 14.98337062 04
| Epoch (UTC): | 24 May 2026 20:47:30 |
| Eccentricity: | 0.0002808 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 292.2278° |
| argument of perigee: | 277.4765° |
| revolutions per day: | 14.98337062 |
| mean anomaly at epoch: | 82.6075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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