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 56200U 26145.57123044 +.00000000 +00000-0 +20346-3 0 00008
2 56200 97.2736 32.5156 0004120 103.5386 256.6312 15.27082521 02
| Epoch (UTC): | 25 May 2026 13:42:34 |
| Eccentricity: | 0.0004120 |
| inclination: | 97.2736° |
| perigee height: | 482 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 32.5156° |
| argument of perigee: | 103.5386° |
| revolutions per day: | 15.27082521 |
| mean anomaly at epoch: | 256.6312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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