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 51741U 26145.54676905 +.00000000 +00000-0 -19035-4 0 00004
2 51741 53.2136 334.1044 0001286 94.3003 265.8136 15.08835293 00
| Epoch (UTC): | 25 May 2026 13:07:20 |
| Eccentricity: | 0.0001286 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.1044° |
| argument of perigee: | 94.3003° |
| revolutions per day: | 15.08835293 |
| mean anomaly at epoch: | 265.8136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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