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 53498U 26145.29315595 +.00000000 +00000-0 -38427-4 0 00008
2 53498 97.4482 266.2963 0001400 171.2562 188.8690 15.05656935 03
| Epoch (UTC): | 25 May 2026 07:02:08 |
| Eccentricity: | 0.0001400 |
| inclination: | 97.4482° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 266.2963° |
| argument of perigee: | 171.2562° |
| revolutions per day: | 15.05656935 |
| mean anomaly at epoch: | 188.8690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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