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 53682U 26145.39838595 +.00000000 +00000-0 -72233-4 0 00007
2 53682 97.4480 26.3923 0002469 85.2078 274.9431 15.05653663 04
| Epoch (UTC): | 25 May 2026 09:33:40 |
| Eccentricity: | 0.0002469 |
| inclination: | 97.4480° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.3923° |
| argument of perigee: | 85.2078° |
| revolutions per day: | 15.05653663 |
| mean anomaly at epoch: | 274.9431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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