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 62499U 26145.55913353 +.00000000 +00000-0 +61442-3 0 00005
2 62499 42.9990 215.2068 0001574 277.0667 83.0006 15.27596751 06
| Epoch (UTC): | 25 May 2026 13:25:09 |
| Eccentricity: | 0.0001574 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.2068° |
| argument of perigee: | 277.0667° |
| revolutions per day: | 15.27596751 |
| mean anomaly at epoch: | 83.0006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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