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 53144U 26145.42483058 +.00000000 +00000-0 -11507-3 0 00000
2 53144 53.2112 189.6516 0001373 94.1462 265.9687 15.08844992 02
| Epoch (UTC): | 25 May 2026 10:11:45 |
| Eccentricity: | 0.0001373 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.6516° |
| argument of perigee: | 94.1462° |
| revolutions per day: | 15.08844992 |
| mean anomaly at epoch: | 265.9687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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