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 53149U 26145.49664938 +.00000000 +00000-0 -20350-4 0 00007
2 53149 53.2159 179.5223 0001826 62.7592 297.3587 15.08837163 09
| Epoch (UTC): | 25 May 2026 11:55:10 |
| Eccentricity: | 0.0001826 |
| inclination: | 53.2159° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.5223° |
| argument of perigee: | 62.7592° |
| revolutions per day: | 15.08837163 |
| mean anomaly at epoch: | 297.3587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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