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 62750U 26145.54118383 +.00000000 +00000-0 +57850-3 0 00002
2 62750 42.9998 80.1250 0000293 267.7697 92.3121 15.27596328 03
| Epoch (UTC): | 25 May 2026 12:59:18 |
| Eccentricity: | 0.0000293 |
| inclination: | 42.9998° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 80.1250° |
| argument of perigee: | 267.7697° |
| revolutions per day: | 15.27596328 |
| mean anomaly at epoch: | 92.3121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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