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 52340U 26145.56053182 +.00000000 +00000-0 -23054-3 0 00003
2 52340 53.2109 214.0338 0001015 93.6873 266.4235 15.08847076 04
| Epoch (UTC): | 25 May 2026 13:27:09 |
| Eccentricity: | 0.0001015 |
| inclination: | 53.2109° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 214.0338° |
| argument of perigee: | 93.6873° |
| revolutions per day: | 15.08847076 |
| mean anomaly at epoch: | 266.4235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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