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 55580U 26145.35395102 +.00000000 +00000-0 +25373-4 0 00006
2 55580 43.0025 266.5888 0001413 268.3358 91.7332 15.27577318 07
| Epoch (UTC): | 25 May 2026 08:29:41 |
| Eccentricity: | 0.0001413 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.5888° |
| argument of perigee: | 268.3358° |
| revolutions per day: | 15.27577318 |
| mean anomaly at epoch: | 91.7332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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