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 51740U 26145.53476662 +.00000000 +00000-0 -77893-4 0 00006
2 51740 53.2137 334.1476 0001550 89.8242 270.2928 15.08845478 02
| Epoch (UTC): | 25 May 2026 12:50:03 |
| Eccentricity: | 0.0001550 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.1476° |
| argument of perigee: | 89.8242° |
| revolutions per day: | 15.08845478 |
| mean anomaly at epoch: | 270.2928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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