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 56138U 26145.49085635 +.00000000 +00000-0 +11370-4 0 00000
2 56138 43.0052 73.4359 0001024 266.3773 93.6962 15.27583912 09
| Epoch (UTC): | 25 May 2026 11:46:49 |
| Eccentricity: | 0.0001024 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.4359° |
| argument of perigee: | 266.3773° |
| revolutions per day: | 15.27583912 |
| mean anomaly at epoch: | 93.6962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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