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 55604U 26145.34238683 +.00000000 +00000-0 -28412-4 0 00000
2 55604 43.0014 266.5078 0001454 261.5798 98.4889 15.27586561 02
| Epoch (UTC): | 25 May 2026 08:13:02 |
| Eccentricity: | 0.0001454 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.5078° |
| argument of perigee: | 261.5798° |
| revolutions per day: | 15.27586561 |
| mean anomaly at epoch: | 98.4889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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