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 56455U 26145.44237508 +.00000000 +00000-0 +30825-4 0 00001
2 56455 69.9990 310.9013 0002859 267.6288 92.4544 14.98328363 04
| Epoch (UTC): | 25 May 2026 10:37:01 |
| Eccentricity: | 0.0002859 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.9013° |
| argument of perigee: | 267.6288° |
| revolutions per day: | 14.98328363 |
| mean anomaly at epoch: | 92.4544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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