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 53500U 26145.66668980 +.00000000 +00000-0 +17191-1 0 00003
2 53500 97.6049 268.7446 0001333 79.7117 162.3130 15.42623672 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001333 |
| inclination: | 97.6049° |
| perigee height: | 437 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 268.7446° |
| argument of perigee: | 79.7117° |
| revolutions per day: | 15.42623672 |
| mean anomaly at epoch: | 162.3130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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