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 62686U 26145.49941360 +.00000000 +00000-0 +11964-3 0 00009
2 62686 97.3973 224.2449 0007441 65.0465 295.1543 15.20907940 03
| Epoch (UTC): | 25 May 2026 11:59:09 |
| Eccentricity: | 0.0007441 |
| inclination: | 97.3973° |
| perigee height: | 498 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 224.2449° |
| argument of perigee: | 65.0465° |
| revolutions per day: | 15.20907940 |
| mean anomaly at epoch: | 295.1543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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