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 51137U 26145.48877043 +.00000000 +00000-0 +86328-5 0 00001
2 51137 53.2139 314.3521 0001264 104.6085 255.5047 15.08831981 00
| Epoch (UTC): | 25 May 2026 11:43:49 |
| Eccentricity: | 0.0001264 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.3521° |
| argument of perigee: | 104.6085° |
| revolutions per day: | 15.08831981 |
| mean anomaly at epoch: | 255.5047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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