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 43753U 26145.64702552 +.00000000 +00000-0 -29726-4 0 00005
2 43753 82.5137 236.1147 0019398 106.6779 253.6432 12.42909054 01
| Epoch (UTC): | 25 May 2026 15:31:43 |
| Eccentricity: | 0.0019398 |
| inclination: | 82.5137° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 236.1147° |
| argument of perigee: | 106.6779° |
| revolutions per day: | 12.42909054 |
| mean anomaly at epoch: | 253.6432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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