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 53023U 26145.30062860 +.00000000 +00000-0 +23705-4 0 00000
2 53023 53.2128 100.1901 0001523 71.6369 288.4789 15.08832986 07
| Epoch (UTC): | 25 May 2026 07:12:54 |
| Eccentricity: | 0.0001523 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.1901° |
| argument of perigee: | 71.6369° |
| revolutions per day: | 15.08832986 |
| mean anomaly at epoch: | 288.4789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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