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 56812U 26145.37785709 +.00000000 +00000-0 +16309-4 0 00002
2 56812 69.9988 130.9837 0003264 266.4886 93.5900 14.98332446 09
| Epoch (UTC): | 25 May 2026 09:04:06 |
| Eccentricity: | 0.0003264 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 130.9837° |
| argument of perigee: | 266.4886° |
| revolutions per day: | 14.98332446 |
| mean anomaly at epoch: | 93.5900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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