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 53775U 26145.66591266 +.00000000 +00000-0 +17576-4 0 00009
2 53775 53.2146 288.7946 0001110 84.2547 275.8572 15.08831218 00
| Epoch (UTC): | 25 May 2026 15:58:54 |
| Eccentricity: | 0.0001110 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 288.7946° |
| argument of perigee: | 84.2547° |
| revolutions per day: | 15.08831218 |
| mean anomaly at epoch: | 275.8572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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