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 51854U 26145.10145065 +.00000000 +00000-0 +99500-3 0 00002
2 51854 53.2153 30.6139 0003410 108.3089 251.8278 15.17354624 04
| Epoch (UTC): | 25 May 2026 02:26:05 |
| Eccentricity: | 0.0003410 |
| inclination: | 53.2153° |
| perigee height: | 511 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 30.6139° |
| argument of perigee: | 108.3089° |
| revolutions per day: | 15.17354624 |
| mean anomaly at epoch: | 251.8278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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