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 51856U 26145.41980365 +.00000000 +00000-0 +15273-4 0 00004
2 51856 53.2132 34.6762 0001104 97.5706 262.5412 15.08843008 00
| Epoch (UTC): | 25 May 2026 10:04:31 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 34.6762° |
| argument of perigee: | 97.5706° |
| revolutions per day: | 15.08843008 |
| mean anomaly at epoch: | 262.5412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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