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 62487U 26087.53951646 +.00000000 +00000-0 +12491-2 0 00001
2 62487 42.9995 182.5844 0001626 274.1785 85.8881 15.27603127 00
| Epoch (UTC): | 28 March 2026 12:56:54 |
| Eccentricity: | 0.0001626 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.5844° |
| argument of perigee: | 274.1785° |
| revolutions per day: | 15.27603127 |
| mean anomaly at epoch: | 85.8881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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