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 55471U 26145.57708897 +.00000000 +00000-0 +11769-4 0 00002
2 55471 43.0028 254.2609 0001638 269.1020 90.9644 15.27575742 04
| Epoch (UTC): | 25 May 2026 13:51:00 |
| Eccentricity: | 0.0001638 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.2609° |
| argument of perigee: | 269.1020° |
| revolutions per day: | 15.27575742 |
| mean anomaly at epoch: | 90.9644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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