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 62281U 26145.35152778 +.00000000 +00000-0 +87269-3 0 00003
2 62281 42.9980 143.6488 0001735 264.8347 95.2306 15.27584238 07
| Epoch (UTC): | 25 May 2026 08:26:12 |
| Eccentricity: | 0.0001735 |
| inclination: | 42.9980° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 143.6488° |
| argument of perigee: | 264.8347° |
| revolutions per day: | 15.27584238 |
| mean anomaly at epoch: | 95.2306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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