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 53612U 26145.26107843 +.00000000 +00000-0 +87716-5 0 00003
2 53612 53.2131 250.4525 0001008 79.8936 280.2170 15.08833117 05
| Epoch (UTC): | 25 May 2026 06:15:57 |
| Eccentricity: | 0.0001008 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 250.4525° |
| argument of perigee: | 79.8936° |
| revolutions per day: | 15.08833117 |
| mean anomaly at epoch: | 280.2170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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