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 53509U 26145.66668980 +.00000000 +00000-0 +33342-2 0 00009
2 53509 97.6029 267.7171 0001390 74.2857 21.2862 15.40290912 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001390 |
| inclination: | 97.6029° |
| perigee height: | 444 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 267.7171° |
| argument of perigee: | 74.2857° |
| revolutions per day: | 15.40290912 |
| mean anomaly at epoch: | 21.2862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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