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 49751U 26145.48047557 +.00000000 +00000-0 -28814-4 0 00005
2 49751 53.2114 164.3171 0001177 76.7313 283.3810 15.08843350 02
| Epoch (UTC): | 25 May 2026 11:31:53 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.3171° |
| argument of perigee: | 76.7313° |
| revolutions per day: | 15.08843350 |
| mean anomaly at epoch: | 283.3810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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