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 55369U 26145.56646344 +.00000000 +00000-0 +24071-4 0 00005
2 55369 43.0021 247.1018 0001455 272.7246 87.3439 15.27575993 05
| Epoch (UTC): | 25 May 2026 13:35:42 |
| Eccentricity: | 0.0001455 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.1018° |
| argument of perigee: | 272.7246° |
| revolutions per day: | 15.27575993 |
| mean anomaly at epoch: | 87.3439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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