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 56201U 26145.58514337 +.00000000 +00000-0 +53291-3 0 00004
2 56201 97.3144 55.1421 0007289 111.5559 248.6467 15.45316140 02
| Epoch (UTC): | 25 May 2026 14:02:36 |
| Eccentricity: | 0.0007289 |
| inclination: | 97.3144° |
| perigee height: | 425 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 55.1421° |
| argument of perigee: | 111.5559° |
| revolutions per day: | 15.45316140 |
| mean anomaly at epoch: | 248.6467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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