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 62731U 26145.61683522 +.00000000 +00000-0 +21849-3 0 00000
2 62731 97.6500 314.6962 0015717 91.1131 269.1900 15.11116806 03
| Epoch (UTC): | 25 May 2026 14:48:14 |
| Eccentricity: | 0.0015717 |
| inclination: | 97.6500° |
| perigee height: | 522 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 314.6962° |
| argument of perigee: | 91.1131° |
| revolutions per day: | 15.11116806 |
| mean anomaly at epoch: | 269.1900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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