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 56103U 26145.19025705 +.00000000 +00000-0 +14807-4 0 00009
2 56103 43.0047 89.3181 0001372 265.0590 95.0105 15.27576976 00
| Epoch (UTC): | 25 May 2026 04:33:58 |
| Eccentricity: | 0.0001372 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 89.3181° |
| argument of perigee: | 265.0590° |
| revolutions per day: | 15.27576976 |
| mean anomaly at epoch: | 95.0105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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