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 53844U 26145.46529416 +.00000000 +00000-0 -34093-4 0 00006
2 53844 53.2159 309.3520 0001627 104.5597 255.5576 15.08842637 09
| Epoch (UTC): | 25 May 2026 11:10:01 |
| Eccentricity: | 0.0001627 |
| inclination: | 53.2159° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.3520° |
| argument of perigee: | 104.5597° |
| revolutions per day: | 15.08842637 |
| mean anomaly at epoch: | 255.5576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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