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 51872U 26145.39401330 +.00000000 +00000-0 +13819-3 0 00002
2 51872 53.2150 24.7819 0001058 84.1978 275.9135 15.08841797 05
| Epoch (UTC): | 25 May 2026 09:27:22 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 24.7819° |
| argument of perigee: | 84.1978° |
| revolutions per day: | 15.08841797 |
| mean anomaly at epoch: | 275.9135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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