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 62493U 26145.49502362 +.00000000 +00000-0 +97768-4 0 00007
2 62493 42.9994 215.5836 0001471 273.2796 86.7887 15.27574977 00
| Epoch (UTC): | 25 May 2026 11:52:50 |
| Eccentricity: | 0.0001471 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.5836° |
| argument of perigee: | 273.2796° |
| revolutions per day: | 15.27574977 |
| mean anomaly at epoch: | 86.7887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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