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 56101U 26145.24793429 +.00000000 +00000-0 +37374-4 0 00002
2 56101 43.0050 88.8903 0001323 268.2477 91.8224 15.27576506 08
| Epoch (UTC): | 25 May 2026 05:57:01 |
| Eccentricity: | 0.0001323 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 88.8903° |
| argument of perigee: | 268.2477° |
| revolutions per day: | 15.27576506 |
| mean anomaly at epoch: | 91.8224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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