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 53672U 26145.39980615 +.00000000 +00000-0 -41236-4 0 00006
2 53672 97.4498 25.3568 0002459 81.4019 278.7486 15.05655784 06
| Epoch (UTC): | 25 May 2026 09:35:43 |
| Eccentricity: | 0.0002459 |
| inclination: | 97.4498° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.3568° |
| argument of perigee: | 81.4019° |
| revolutions per day: | 15.05655784 |
| mean anomaly at epoch: | 278.7486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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