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 52349U 26145.41700634 +.00000000 +00000-0 -55044-5 0 00003
2 52349 53.2107 214.6783 0001353 90.9909 269.1239 15.08839540 07
| Epoch (UTC): | 25 May 2026 10:00:29 |
| Eccentricity: | 0.0001353 |
| inclination: | 53.2107° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.6783° |
| argument of perigee: | 90.9909° |
| revolutions per day: | 15.08839540 |
| mean anomaly at epoch: | 269.1239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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