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 45754U 26145.48510971 +.00000000 +00000-0 +14134-2 0 00006
2 45754 53.0471 222.8391 0000702 315.4496 44.6441 15.18213842 03
| Epoch (UTC): | 25 May 2026 11:38:33 |
| Eccentricity: | 0.0000702 |
| inclination: | 53.0471° |
| perigee height: | 511 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 222.8391° |
| argument of perigee: | 315.4496° |
| revolutions per day: | 15.18213842 |
| mean anomaly at epoch: | 44.6441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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