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 45100U 26145.57144861 +.00000000 +00000-0 +42039-3 0 00008
2 45100 53.0466 214.9594 0003839 293.4931 66.5681 15.66427871 03
| Epoch (UTC): | 25 May 2026 13:42:53 |
| Eccentricity: | 0.0003839 |
| inclination: | 53.0466° |
| perigee height: | 367 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 214.9594° |
| argument of perigee: | 293.4931° |
| revolutions per day: | 15.66427871 |
| mean anomaly at epoch: | 66.5681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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