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 62977U 26145.55618961 +.00000000 +00000-0 +65400-4 0 00002
2 62977 50.0073 316.7542 0001230 94.3141 265.7872 13.29325214 03
| Epoch (UTC): | 25 May 2026 13:20:54 |
| Eccentricity: | 0.0001230 |
| inclination: | 50.0073° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 316.7542° |
| argument of perigee: | 94.3141° |
| revolutions per day: | 13.29325214 |
| mean anomaly at epoch: | 265.7872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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