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 53649U 26145.66668980 +.00000000 +00000-0 +25030-2 0 00009
2 53649 97.6029 28.6049 0001988 74.6299 100.0370 15.35625302 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001988 |
| inclination: | 97.6029° |
| perigee height: | 458 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 28.6049° |
| argument of perigee: | 74.6299° |
| revolutions per day: | 15.35625302 |
| mean anomaly at epoch: | 100.0370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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