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 55983U 26145.53793362 +.00000000 +00000-0 +37747-3 0 00000
2 55983 42.0018 333.5579 0006609 206.0238 154.0270 15.38569010 01
| Epoch (UTC): | 25 May 2026 12:54:37 |
| Eccentricity: | 0.0006609 |
| inclination: | 42.0018° |
| perigee height: | 446 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 333.5579° |
| argument of perigee: | 206.0238° |
| revolutions per day: | 15.38569010 |
| mean anomaly at epoch: | 154.0270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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