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 53268U 26145.55914487 +.00000000 +00000-0 +72009-4 0 00000
2 53268 53.2144 209.0417 0000629 51.9425 308.1624 15.08842403 00
| Epoch (UTC): | 25 May 2026 13:25:10 |
| Eccentricity: | 0.0000629 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.0417° |
| argument of perigee: | 51.9425° |
| revolutions per day: | 15.08842403 |
| mean anomaly at epoch: | 308.1624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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