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 53043U 26145.40394777 +.00000000 +00000-0 -89692-4 0 00006
2 53043 97.4460 325.2870 0001067 97.2737 262.8612 15.05661027 03
| Epoch (UTC): | 25 May 2026 09:41:41 |
| Eccentricity: | 0.0001067 |
| inclination: | 97.4460° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.2870° |
| argument of perigee: | 97.2737° |
| revolutions per day: | 15.05661027 |
| mean anomaly at epoch: | 262.8612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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