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 53564U 26145.52419672 +.00000000 +00000-0 -78192-5 0 00003
2 53564 53.2138 69.2631 0001196 93.4757 266.6372 15.08836118 09
| Epoch (UTC): | 25 May 2026 12:34:50 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.2631° |
| argument of perigee: | 93.4757° |
| revolutions per day: | 15.08836118 |
| mean anomaly at epoch: | 266.6372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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