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 52464U 26145.51085985 +.00000000 +00000-0 +54069-3 0 00000
2 52464 53.2147 74.2578 0001690 94.2566 265.8619 15.08802812 08
| Epoch (UTC): | 25 May 2026 12:15:38 |
| Eccentricity: | 0.0001690 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.2578° |
| argument of perigee: | 94.2566° |
| revolutions per day: | 15.08802812 |
| mean anomaly at epoch: | 265.8619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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