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 53277U 26145.39079488 +.00000000 +00000-0 -15634-4 0 00007
2 53277 53.2125 199.8228 0001463 72.8791 287.2361 15.08845836 08
| Epoch (UTC): | 25 May 2026 09:22:44 |
| Eccentricity: | 0.0001463 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.8228° |
| argument of perigee: | 72.8791° |
| revolutions per day: | 15.08845836 |
| mean anomaly at epoch: | 287.2361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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