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 55351U 26145.57002889 +.00000000 +00000-0 +20513-4 0 00004
2 55351 43.0022 229.0145 0001562 264.7662 95.3011 15.27576843 09
| Epoch (UTC): | 25 May 2026 13:40:50 |
| Eccentricity: | 0.0001562 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.0145° |
| argument of perigee: | 264.7662° |
| revolutions per day: | 15.27576843 |
| mean anomaly at epoch: | 95.3011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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