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 53528U 26145.55179549 +.00000000 +00000-0 +43849-5 0 00002
2 53528 53.2124 89.0740 0001241 92.2342 267.8792 15.08834671 04
| Epoch (UTC): | 25 May 2026 13:14:35 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 89.0740° |
| argument of perigee: | 92.2342° |
| revolutions per day: | 15.08834671 |
| mean anomaly at epoch: | 267.8792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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