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 51114U 26145.47864720 +.00000000 +00000-0 +22414-4 0 00008
2 51114 53.2126 304.4003 0001298 98.8085 261.3054 15.08842193 07
| Epoch (UTC): | 25 May 2026 11:29:15 |
| Eccentricity: | 0.0001298 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.4003° |
| argument of perigee: | 98.8085° |
| revolutions per day: | 15.08842193 |
| mean anomaly at epoch: | 261.3054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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