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 51116U 26145.46488205 +.00000000 +00000-0 -37253-4 0 00007
2 51116 53.2125 304.4343 0001232 92.7589 267.3544 15.08836418 08
| Epoch (UTC): | 25 May 2026 11:09:25 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.4343° |
| argument of perigee: | 92.7589° |
| revolutions per day: | 15.08836418 |
| mean anomaly at epoch: | 267.3544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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