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 51727U 26145.54857164 +.00000000 +00000-0 -15505-4 0 00004
2 51727 53.2130 344.0845 0001096 87.5778 272.5340 15.08837630 08
| Epoch (UTC): | 25 May 2026 13:09:56 |
| Eccentricity: | 0.0001096 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 344.0845° |
| argument of perigee: | 87.5778° |
| revolutions per day: | 15.08837630 |
| mean anomaly at epoch: | 272.5340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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