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 55623U 26145.50003470 +.00000000 +00000-0 -56425-3 0 00007
2 55623 43.0021 280.4942 0001477 266.6548 173.3135 15.27576919 03
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001477 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.4942° |
| argument of perigee: | 266.6548° |
| revolutions per day: | 15.27576919 |
| mean anomaly at epoch: | 173.3135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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