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 45710U 26145.35177187 +.00000000 +00000-0 +50122-3 0 00000
2 45710 53.0453 7.9322 0007059 65.3006 294.8744 15.67420699 00
| Epoch (UTC): | 25 May 2026 08:26:33 |
| Eccentricity: | 0.0007059 |
| inclination: | 53.0453° |
| perigee height: | 362 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 7.9322° |
| argument of perigee: | 65.3006° |
| revolutions per day: | 15.67420699 |
| mean anomaly at epoch: | 294.8744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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