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 56335U 26145.47315418 +.00000000 +00000-0 +70404-4 0 00005
2 56335 97.4491 146.5789 0002036 114.3607 245.7833 15.05652757 06
| Epoch (UTC): | 25 May 2026 11:21:20 |
| Eccentricity: | 0.0002036 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.5789° |
| argument of perigee: | 114.3607° |
| revolutions per day: | 15.05652757 |
| mean anomaly at epoch: | 245.7833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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