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 51749U 26145.24406887 +.00000000 +00000-0 +58172-4 0 00003
2 51749 53.2143 335.6340 0001232 83.0931 277.0201 15.08840664 03
| Epoch (UTC): | 25 May 2026 05:51:27 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 335.6340° |
| argument of perigee: | 83.0931° |
| revolutions per day: | 15.08840664 |
| mean anomaly at epoch: | 277.0201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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