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 57714U 26145.12724904 +.00000000 +00000-0 +11834-3 0 00004
2 57714 43.0055 49.5378 0001576 243.5618 116.5072 15.27598503 04
| Epoch (UTC): | 25 May 2026 03:03:14 |
| Eccentricity: | 0.0001576 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.5378° |
| argument of perigee: | 243.5618° |
| revolutions per day: | 15.27598503 |
| mean anomaly at epoch: | 116.5072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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