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 53803U 26145.04809462 +.00000000 +00000-0 +30674-4 0 00007
2 53803 53.2165 266.3768 0000762 94.4692 265.6387 15.08836883 07
| Epoch (UTC): | 25 May 2026 01:09:15 |
| Eccentricity: | 0.0000762 |
| inclination: | 53.2165° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 266.3768° |
| argument of perigee: | 94.4692° |
| revolutions per day: | 15.08836883 |
| mean anomaly at epoch: | 265.6387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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