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 51739U 26145.48692742 +.00000000 +00000-0 -24938-3 0 00008
2 51739 53.2132 334.3644 0001092 91.8361 268.2756 15.08860995 07
| Epoch (UTC): | 25 May 2026 11:41:10 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 334.3644° |
| argument of perigee: | 91.8361° |
| revolutions per day: | 15.08860995 |
| mean anomaly at epoch: | 268.2756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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