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 56377U 26145.32171816 +.00000000 +00000-0 +14638-3 0 00003
2 56377 43.0016 125.6321 0000506 307.7155 52.3651 15.27584615 09
| Epoch (UTC): | 25 May 2026 07:43:16 |
| Eccentricity: | 0.0000506 |
| inclination: | 43.0016° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 125.6321° |
| argument of perigee: | 307.7155° |
| revolutions per day: | 15.27584615 |
| mean anomaly at epoch: | 52.3651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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