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 56712U 26145.48575352 +.00000000 +00000-0 +16317-3 0 00002
2 56712 87.9108 233.2853 0002301 94.9884 265.1509 13.16595889 03
| Epoch (UTC): | 25 May 2026 11:39:29 |
| Eccentricity: | 0.0002301 |
| inclination: | 87.9108° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2853° |
| argument of perigee: | 94.9884° |
| revolutions per day: | 13.16595889 |
| mean anomaly at epoch: | 265.1509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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