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 57652U 26145.04378704 +.00000000 +00000-0 +10197-3 0 00000
2 57652 43.0060 21.3505 0001618 261.4958 98.5711 15.27575242 08
| Epoch (UTC): | 25 May 2026 01:03:03 |
| Eccentricity: | 0.0001618 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.3505° |
| argument of perigee: | 261.4958° |
| revolutions per day: | 15.27575242 |
| mean anomaly at epoch: | 98.5711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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